getting unexpeted result while performing linear density triangular pannel methd ; could't figureout the exact bug why this is happening what i am doing wrong

Questions, suggestions, feature requests, bug reports, feedbackCategory: Questionsgetting unexpeted result while performing linear density triangular pannel methd ; could't figureout the exact bug why this is happening what i am doing wrong
Abhishek RaiAbhishek Rai asked 1 month ago

flow5 v7.01_beta_07
13 June 2020 23:08:31
Launching analysis
Initializing task
Plane Name
Checking plane and polar data
…done
Initializing the triangle analysis
Connecting triangular panels
Time to make the triangle connections: 0.114 s
T2-TriLinear-ThickSurf
Type 2 – Fixed lift polar
Density = 1.225kg/m3
Viscosity = 1.5e-05m²/s
RFF = 10.0
Core radius = 0.001mm
Running in multi-threaded mode
Linear system calculations in floating point double precision
Using S. Nintcheu-Fata’s method for off-plane integrals
Allocating 485.00Mb for the influence matrix
Allocating 8.65Mb for 31 RHS vectors
Linear density triangular panels
Counted 2660 triangular panels
Matrix size = 7980
Computing quadratures at order 5
Allocating result arrays
Locking objects
Setting inertia
Mass= 5.045 kg
___Center of Gravity Position – Body axis____
CoG_x= 0.0517 m
CoG_y= -0.0000 m
CoG_z= 0.0008 m
___Inertia – Body Axis – CoG Origin____
Ibxx= 0.1272 kg.m²
Ibyy= 0.2128 kg.m²
Ibzz= 0.3393 kg.m²
Ibxz= -0.0013 kg.m²
Solving the problem…
Making the unit RHS vectors…
Time to make the RHS vectors: 1.20 s
Making the influence matrix…
Time to make the influence matrix: 2.08 s
Adding the wake’s contributions…
Time to make the wake contributions: 0.40 s
LAPACK – LU decomposition…
Factorizing LU…
Time to solve the linear system: 1.319 s
Making the unit local panel velocities …
Computing on-body pressure coefficients…
Creating source strengths…
Calculating doublet strengths…
Calculating far field forces…
Alpha=-5.00° QInf=13.55 m/s
Alpha=-4.50° QInf=11.12 m/s
Alpha=-4.00° QInf= 9.64 m/s
Alpha=-3.50° QInf= 8.62 m/s
Alpha=-3.00° QInf= 7.87 m/s
Alpha=-2.50° QInf= 7.30 m/s
Alpha=-2.00° QInf= 6.84 m/s
Alpha=-1.50° QInf= 6.47 m/s
Alpha=-1.00° QInf= 6.17 m/s
Alpha=-0.50° QInf= 5.93 m/s
Alpha= 0.00° QInf= 5.72 m/s
Alpha= 0.50° QInf= 5.55 m/s
Alpha= 1.00° QInf= 5.41 m/s
Alpha= 1.50° QInf= 5.30 m/s
Alpha= 2.00° QInf= 5.22 m/s
Alpha= 2.50° QInf= 5.16 m/s
Alpha= 3.00° QInf= 5.12 m/s
Alpha= 3.50° QInf= 5.11 m/s
Alpha= 4.00° QInf= 5.12 m/s
Alpha= 4.50° QInf= 5.15 m/s
Alpha= 5.00° QInf= 5.22 m/s
Alpha= 5.50° QInf= 5.32 m/s
Alpha= 6.00° QInf= 5.46 m/s
Alpha= 6.50° QInf= 5.66 m/s
Alpha= 7.00° QInf= 5.93 m/s
Alpha= 7.50° QInf= 6.32 m/s
Alpha= 8.00° QInf= 6.87 m/s
Alpha= 8.50° QInf= 7.72 m/s
Alpha= 9.00° QInf= 9.23 m/s
Alpha= 9.50° QInf=12.79 m/s
Found a negative lift for Alpha=10.00° …. skipping the angle…
Computing Plane for alpha=-5.00° beta=0.00°
Calculating aerodynamic coefficients…
Calculating Main Wing
Interpolating viscous properties …
Span position -190.05 mm, Re = 202250, AoA_effective = 35.26° could not be interpolated
Span position -149.48 mm, Re = 207291, AoA_effective = 74.40° could not be interpolated
Span position -113.34 mm, Re = 211779, AoA_effective = 83.49° could not be interpolated
Span position -81.90 mm, Re = 215685, AoA_effective = 83.07° could not be interpolated
Span position -55.36 mm, Re = 218982, AoA_effective = 79.89° could not be interpolated
Span position -33.91 mm, Re = 221646, AoA_effective = 75.97° could not be interpolated
Span position -17.70 mm, Re = 223661, AoA_effective = 72.63° could not be interpolated
Span position -6.82 mm, Re = 225012, AoA_effective = 70.49° could not be interpolated
Span position -1.37 mm, Re = 225689, AoA_effective = 69.59° could not be interpolated
Span position 1.37 mm, Re = 225689, AoA_effective = 69.59° could not be interpolated
Span position 6.82 mm, Re = 225012, AoA_effective = 70.49° could not be interpolated
Span position 17.70 mm, Re = 223661, AoA_effective = 72.64° could not be interpolated
Span position 33.91 mm, Re = 221646, AoA_effective = 75.98° could not be interpolated
Span position 55.36 mm, Re = 218982, AoA_effective = 79.89° could not be interpolated
Span position 81.90 mm, Re = 215685, AoA_effective = 83.07° could not be interpolated
Span position 113.34 mm, Re = 211779, AoA_effective = 83.49° could not be interpolated
Span position 149.48 mm, Re = 207291, AoA_effective = 74.38° could not be interpolated
Span position 190.05 mm, Re = 202250, AoA_effective = 35.23° could not be interpolated
Calculating Elevator
Interpolating viscous properties …
Span position -177.75 mm, Re = 132512, AoA_effective = -51.76° could not be interpolated
Span position -134.36 mm, Re = 144272, AoA_effective = -69.55° could not be interpolated
Span position -94.26 mm, Re = 155139, AoA_effective = -65.51° could not be interpolated
Span position -59.47 mm, Re = 164570, AoA_effective = -57.37° could not be interpolated
Span position -31.72 mm, Re = 172090, AoA_effective = -49.84° could not be interpolated
Span position -12.41 mm, Re = 177324, AoA_effective = -44.46° could not be interpolated
Span position -2.51 mm, Re = 180008, AoA_effective = -41.66° could not be interpolated
Span position 2.51 mm, Re = 180008, AoA_effective = -41.66° could not be interpolated
Span position 12.41 mm, Re = 177324, AoA_effective = -44.47° could not be interpolated
Span position 31.72 mm, Re = 172090, AoA_effective = -49.85° could not be interpolated
Span position 59.47 mm, Re = 164570, AoA_effective = -57.38° could not be interpolated
Span position 94.26 mm, Re = 155139, AoA_effective = -65.51° could not be interpolated
Span position 134.36 mm, Re = 144272, AoA_effective = -69.55° could not be interpolated
Span position 177.75 mm, Re = 132512, AoA_effective = -51.76° could not be interpolated
Calculating Fin
Interpolating viscous properties …
Computing Plane for alpha=-4.50° beta=0.00°
Calculating aerodynamic coefficients…
Calculating Main Wing
Interpolating viscous properties …
Span position -190.05 mm, Re = 165982, AoA_effective = 78.06° could not be interpolated
Span position -149.48 mm, Re = 170119, AoA_effective = 160.52° could not be interpolated
Span position -113.34 mm, Re = 173803, AoA_effective = 179.47° could not be interpolated
Span position -81.90 mm, Re = 177008, AoA_effective = 178.39° could not be interpolated
Span position -55.36 mm, Re = 179713, AoA_effective = 171.58° could not be interpolated
Span position -33.91 mm, Re = 181900, AoA_effective = 163.27° could not be interpolated
Span position -17.70 mm, Re = 183554, AoA_effective = 156.21° could not be interpolated
Span position -6.82 mm, Re = 184662, AoA_effective = 151.68° could not be interpolated
Span position -1.37 mm, Re = 185218, AoA_effective = 149.78° could not be interpolated
Span position 1.37 mm, Re = 185218, AoA_effective = 149.79° could not be interpolated
Span position 6.82 mm, Re = 184662, AoA_effective = 151.69° could not be interpolated
Span position 17.70 mm, Re = 183554, AoA_effective = 156.23° could not be interpolated
Span position 33.91 mm, Re = 181900, AoA_effective = 163.29° could not be interpolated
Span position 55.36 mm, Re = 179713, AoA_effective = 171.59° could not be interpolated
Span position 81.90 mm, Re = 177008, AoA_effective = 178.40° could not be interpolated
Span position 113.34 mm, Re = 173803, AoA_effective = 179.46° could not be interpolated
Span position 149.48 mm, Re = 170119, AoA_effective = 160.48° could not be interpolated
Span position 190.05 mm, Re = 165982, AoA_effective = 77.99° could not be interpolated
Calculating Elevator
Interpolating viscous properties …
Span position -177.75 mm, Re = 108750, AoA_effective = -130.67° could not be interpolated
Span position -134.36 mm, Re = 118401, AoA_effective = -179.06° could not be interpolated
Span position -94.26 mm, Re = 127319, AoA_effective = -172.60° could not be interpolated
Span position -59.47 mm, Re = 135059, AoA_effective = -154.90° could not be interpolated
Span position -31.72 mm, Re = 141231, AoA_effective = -137.47° could not be interpolated
Span position -12.41 mm, Re = 145526, AoA_effective = -124.92° could not be interpolated
Span position -2.51 mm, Re = 147728, AoA_effective = -118.44° could not be interpolated
Span position 2.51 mm, Re = 147728, AoA_effective = -118.44° could not be interpolated
Span position 12.41 mm, Re = 145526, AoA_effective = -124.95° could not be interpolated
Span position 31.72 mm, Re = 141231, AoA_effective = -137.50° could not be interpolated
Span position 59.47 mm, Re = 135059, AoA_effective = -154.92° could not be interpolated
Span position 94.26 mm, Re = 127319, AoA_effective = -172.61° could not be interpolated
Span position 134.36 mm, Re = 118401, AoA_effective = -179.07° could not be interpolated
Span position 177.75 mm, Re = 108750, AoA_effective = -130.68° could not be interpolated
Calculating Fin
Interpolating viscous properties …
Computing Plane for alpha=-4.00° beta=0.00°
Calculating aerodynamic coefficients…
Calculating Main Wing
Interpolating viscous properties …
Span position -190.05 mm, Re = 143846, AoA_effective = 136.42° could not be interpolated
Span position -149.48 mm, Re = 147431, AoA_effective = 278.16° could not be interpolated
Span position -113.34 mm, Re = 150623, AoA_effective = 310.53° could not be interpolated
Span position -81.90 mm, Re = 153401, AoA_effective = 308.50° could not be interpolated
Span position -55.36 mm, Re = 155746, AoA_effective = 296.68° could not be interpolated
Span position -33.91 mm, Re = 157641, AoA_effective = 282.35° could not be interpolated
Span position -17.70 mm, Re = 159074, AoA_effective = 270.20° could not be interpolated
Span position -6.82 mm, Re = 160035, AoA_effective = 262.40° could not be interpolated
Span position -1.37 mm, Re = 160517, AoA_effective = 259.13° could not be interpolated
Span position 1.37 mm, Re = 160517, AoA_effective = 259.14° could not be interpolated
Span position 6.82 mm, Re = 160035, AoA_effective = 262.41° could not be interpolated
Span position 17.70 mm, Re = 159074, AoA_effective = 270.22° could not be interpolated
Span position 33.91 mm, Re = 157641, AoA_effective = 282.38° could not be interpolated
Span position 55.36 mm, Re = 155746, AoA_effective = 296.70° could not be interpolated
Span position 81.90 mm, Re = 153401, AoA_effective = 308.51° could not be interpolated
Span position 113.34 mm, Re = 150623, AoA_effective = 310.52° could not be interpolated
Span position 149.48 mm, Re = 147431, AoA_effective = 278.09° could not be interpolated
Span position 190.05 mm, Re = 143846, AoA_effective = 136.31° could not be interpolated
Calculating Elevator
Interpolating viscous properties …
Span position -177.75 mm, Re = 94246, AoA_effective = -244.44° could not be interpolated
Span position -134.36 mm, Re = 102610, AoA_effective = -337.71° could not be interpolated
Span position -94.26 mm, Re = 110339, AoA_effective = -328.49° could not be interpolated
Span position -59.47 mm, Re = 117047, AoA_effective = -297.42° could not be interpolated
Span position -31.72 mm, Re = 122395, AoA_effective = -265.99° could not be interpolated
Span position -12.41 mm, Re = 126118, AoA_effective = -243.14° could not be interpolated
Span position -2.51 mm, Re = 128027, AoA_effective = -231.36° could not be interpolated
Span position 2.51 mm, Re = 128027, AoA_effective = -231.37° could not be interpolated
Span position 12.41 mm, Re = 126118, AoA_effective = -243.19° could not be interpolated
Span position 31.72 mm, Re = 122395, AoA_effective = -266.05° could not be interpolated
Span position 59.47 mm, Re = 117047, AoA_effective = -297.46° could not be interpolated
Span position 94.26 mm, Re = 110339, AoA_effective = -328.51° could not be interpolated
Span position 134.36 mm, Re = 102610, AoA_effective = -337.72° could not be interpolated
Span position 177.75 mm, Re = 94246, AoA_effective = -244.45° could not be interpolated
Calculating Fin
Interpolating viscous properties …
Computing Plane for alpha=-3.50° beta=0.00°
Calculating aerodynamic coefficients…
Calculating Main Wing
Interpolating viscous properties …
Span position -190.05 mm, Re = 128645, AoA_effective = 210.31° could not be interpolated
Span position -149.48 mm, Re = 131852, AoA_effective = 427.26° could not be interpolated
Span position -113.34 mm, Re = 134707, AoA_effective = 476.62° could not be interpolated
Span position -81.90 mm, Re = 137191, AoA_effective = 473.36° could not be interpolated
Span position -55.36 mm, Re = 139288, AoA_effective = 455.16° could not be interpolated
Span position -33.91 mm, Re = 140983, AoA_effective = 433.18° could not be interpolated
Span position -17.70 mm, Re = 142264, AoA_effective = 414.55° could not be interpolated
Span position -6.82 mm, Re = 143123, AoA_effective = 402.61° could not be interpolated
Span position -1.37 mm, Re = 143554, AoA_effective = 397.61° could not be interpolated
Span position 1.37 mm, Re = 143554, AoA_effective = 397.62° could not be interpolated
Span position 6.82 mm, Re = 143123, AoA_effective = 402.63° could not be interpolated
Span position 17.70 mm, Re = 142264, AoA_effective = 414.59° could not be interpolated
Span position 33.91 mm, Re = 140983, AoA_effective = 433.22° could not be interpolated
Span position 55.36 mm, Re = 139288, AoA_effective = 455.19° could not be interpolated
Span position 81.90 mm, Re = 137191, AoA_effective = 473.36° could not be interpolated
Span position 113.34 mm, Re = 134707, AoA_effective = 476.61° could not be interpolated
Span position 149.48 mm, Re = 131852, AoA_effective = 427.15° could not be interpolated
Span position 190.05 mm, Re = 128645, AoA_effective = 210.14° could not be interpolated
Calculating Elevator
Interpolating viscous properties …
Span position -177.75 mm, Re = 84287, AoA_effective = -393.04° could not be interpolated
Span position -134.36 mm, Re = 91767, AoA_effective = -545.37° could not be interpolated
Span position -94.26 mm, Re = 98680, AoA_effective = -533.06° could not be interpolated
Span position -59.47 mm, Re = 104678, AoA_effective = -484.89° could not be interpolated
Span position -31.72 mm, Re = 109462, AoA_effective = -435.44° could not be interpolated
Span position -12.41 mm, Re = 112790, AoA_effective = -399.34° could not be interpolated
Span position -2.51 mm, Re = 114498, AoA_effective = -380.79° could not be interpolated
Span position 2.51 mm, Re = 114498, AoA_effective = -380.80° could not be interpolated
Span position 12.41 mm, Re = 112790, AoA_effective = -399.42° could not be interpolated
Span position 31.72 mm, Re = 109462, AoA_effective = -435.52° could not be interpolated
Span position 59.47 mm, Re = 104678, AoA_effective = -484.95° could not be interpolated
Span position 94.26 mm, Re = 98680, AoA_effective = -533.10° could not be interpolated
Span position 134.36 mm, Re = 91767, AoA_effective = -545.40° could not be interpolated
Span position 177.75 mm, Re = 84287, AoA_effective = -393.05° could not be interpolated
Calculating Fin
Interpolating viscous properties …
Computing Plane for alpha=-3.00° beta=0.00°
Calculating aerodynamic coefficients…
Calculating Main Wing
Interpolating viscous properties …
Span position -190.05 mm, Re = 117469, AoA_effective = 299.68° could not be interpolated
Span position -149.48 mm, Re = 120397, AoA_effective = 607.71° could not be interpolated
Span position -113.34 mm, Re = 123004, AoA_effective = 677.64° could not be interpolated
Span position -81.90 mm, Re = 125273, AoA_effective = 672.86° could not be interpolated
Span position -55.36 mm, Re = 127187, AoA_effective = 646.94° could not be interpolated
Span position -33.91 mm, Re = 128735, AoA_effective = 615.68° could not be interpolated
Span position -17.70 mm, Re = 129905, AoA_effective = 589.22° could not be interpolated
Span position -6.82 mm, Re = 130690, AoA_effective = 572.26° could not be interpolated
Span position -1.37 mm, Re = 131083, AoA_effective = 565.16° could not be interpolated
Span position 1.37 mm, Re = 131083, AoA_effective = 565.18° could not be interpolated
Span position 6.82 mm, Re = 130690, AoA_effective = 572.29° could not be interpolated
Span position 17.70 mm, Re = 129905, AoA_effective = 589.28° could not be interpolated
Span position 33.91 mm, Re = 128735, AoA_effective = 615.74° could not be interpolated
Span position 55.36 mm, Re = 127187, AoA_effective = 646.98° could not be interpolated
Span position 81.90 mm, Re = 125273, AoA_effective = 672.87° could not be interpolated
Span position 113.34 mm, Re = 123004, AoA_effective = 677.62° could not be interpolated
Span position 149.48 mm, Re = 120397, AoA_effective = 607.56° could not be interpolated
Span position 190.05 mm, Re = 117469, AoA_effective = 299.43° could not be interpolated
Calculating Elevator
Interpolating viscous properties …
Span position -177.75 mm, Re = 76965, AoA_effective = -576.40° could not be interpolated
Span position -134.36 mm, Re = 83795, AoA_effective = -801.99° could not be interpolated
Span position -94.26 mm, Re = 90107, AoA_effective = -786.25° could not be interpolated
Span position -59.47 mm, Re = 95584, AoA_effective = -717.25° could not be interpolated
Span position -31.72 mm, Re = 99952, AoA_effective = -645.72° could not be interpolated
Span position -12.41 mm, Re = 102992, AoA_effective = -593.41° could not be interpolated
Span position -2.51 mm, Re = 104551, AoA_effective = -566.54° could not be interpolated
Span position 2.51 mm, Re = 104551, AoA_effective = -566.56° could not be interpolated
Span position 12.41 mm, Re = 102992, AoA_effective = -593.52° could not be interpolated
Span position 31.72 mm, Re = 99952, AoA_effective = -645.84° could not be interpolated
Span position 59.47 mm, Re = 95584, AoA_effective = -717.33° could not be interpolated
Span position 94.26 mm, Re = 90107, AoA_effective = -786.29° could not be interpolated
Span position 134.36 mm, Re = 83795, AoA_effective = -802.03° could not be interpolated
Span position 177.75 mm, Re = 76965, AoA_effective = -576.42° could not be interpolated
Calculating Fin
Interpolating viscous properties …
Computing Plane for alpha=-2.50° beta=0.00°
Calculating aerodynamic coefficients…
Calculating Main Wing
Interpolating viscous properties …
Span position -190.05 mm, Re = 108885, AoA_effective = 404.60° could not be interpolated
Span position -149.48 mm, Re = 111598, AoA_effective = 819.60° could not be interpolated
Span position -113.34 mm, Re = 114015, AoA_effective = 913.61° could not be interpolated
Span position -81.90 mm, Re = 116118, AoA_effective = 906.99° could not be interpolated
Span position -55.36 mm, Re = 117892, AoA_effective = 871.96° could not be interpolated
Span position -33.91 mm, Re = 119327, AoA_effective = 829.78° could not be interpolated
Span position -17.70 mm, Re = 120412, AoA_effective = 794.11° could not be interpolated
Span position -6.82 mm, Re = 121139, AoA_effective = 771.25° could not be interpolated
Span position -1.37 mm, Re = 121504, AoA_effective = 761.69° could not be interpolated
Span position 1.37 mm, Re = 121504, AoA_effective = 761.71° could not be interpolated
Span position 6.82 mm, Re = 121139, AoA_effective = 771.29° could not be interpolated
Span position 17.70 mm, Re = 120412, AoA_effective = 794.18° could not be interpolated
Span position 33.91 mm, Re = 119327, AoA_effective = 829.86° could not be interpolated
Span position 55.36 mm, Re = 117892, AoA_effective = 872.02° could not be interpolated
Span position 81.90 mm, Re = 116118, AoA_effective = 907.01° could not be interpolated
Span position 113.34 mm, Re = 114015, AoA_effective = 913.60° could not be interpolated
Span position 149.48 mm, Re = 111598, AoA_effective = 819.40° could not be interpolated
Span position 190.05 mm, Re = 108885, AoA_effective = 404.27° could not be interpolated
Calculating Elevator
Interpolating viscous properties …
Span position -177.75 mm, Re = 71340, AoA_effective = -794.49° could not be interpolated
Span position -134.36 mm, Re = 77671, AoA_effective = -1107.48° could not be interpolated
Span position -94.26 mm, Re = 83522, AoA_effective = -1087.96° could not be interpolated
Span position -59.47 mm, Re = 88599, AoA_effective = -994.43° could not be interpolated
Span position -31.72 mm, Re = 92648, AoA_effective = -896.79° could not be interpolated
Span position -12.41 mm, Re = 95465, AoA_effective = -825.27° could not be interpolated
Span position -2.51 mm, Re = 96910, AoA_effective = -788.56° could not be interpolated
Span position 2.51 mm, Re = 96910, AoA_effective = -788.59° could not be interpolated
Span position 12.41 mm, Re = 95465, AoA_effective = -825.42° could not be interpolated
Span position 31.72 mm, Re = 92648, AoA_effective = -896.95° could not be interpolated
Span position 59.47 mm, Re = 88599, AoA_effective = -994.54° could not be interpolated
Span position 94.26 mm, Re = 83522, AoA_effective = -1088.03° could not be interpolated
Span position 134.36 mm, Re = 77671, AoA_effective = -1107.53° could not be interpolated
Span position 177.75 mm, Re = 71340, AoA_effective = -794.51° could not be interpolated
Calculating Fin
Interpolating viscous properties …
Computing Plane for alpha=-2.00° beta=0.00°
Calculating aerodynamic coefficients…
Calculating Main Wing
Interpolating viscous properties …
Span position -190.05 mm, Re = 102093, AoA_effective = 524.98° could not be interpolated
Span position -149.48 mm, Re = 104638, AoA_effective = 1062.79° could not be interpolated
Span position -113.34 mm, Re = 106904, AoA_effective = 1184.45° could not be interpolated
Span position -81.90 mm, Re = 108875, AoA_effective = 1175.72° could not be interpolated
Span position -55.36 mm, Re = 110539, AoA_effective = 1130.23° could not be interpolated
Span position -33.91 mm, Re = 111884, AoA_effective = 1075.53° could not be interpolated
Span position -17.70 mm, Re = 112901, AoA_effective = 1029.28° could not be interpolated
Span position -6.82 mm, Re = 113583, AoA_effective = 999.64° could not be interpolated
Span position -1.37 mm, Re = 113925, AoA_effective = 987.25° could not be interpolated
Span position 1.37 mm, Re = 113925, AoA_effective = 987.27° could not be interpolated
Span position 6.82 mm, Re = 113583, AoA_effective = 999.68° could not be interpolated
Span position 17.70 mm, Re = 112901, AoA_effective = 1029.37° could not be interpolated
Span position 33.91 mm, Re = 111884, AoA_effective = 1075.63° could not be interpolated
Span position 55.36 mm, Re = 110539, AoA_effective = 1130.31° could not be interpolated
Span position 81.90 mm, Re = 108875, AoA_effective = 1175.74° could not be interpolated
Span position 113.34 mm, Re = 106904, AoA_effective = 1184.43° could not be interpolated
Span position 149.48 mm, Re = 104638, AoA_effective = 1062.53° could not be interpolated
Span position 190.05 mm, Re = 102093, AoA_effective = 524.55° could not be interpolated
Calculating Elevator
Interpolating viscous properties …
Span position -177.75 mm, Re = 66890, AoA_effective = -1047.23° could not be interpolated
Span position -134.36 mm, Re = 72827, AoA_effective = -1461.76° could not be interpolated
Span position -94.26 mm, Re = 78312, AoA_effective = -1438.13° could not be interpolated
Span position -59.47 mm, Re = 83073, AoA_effective = -1316.34° could not be interpolated
Span position -31.72 mm, Re = 86869, AoA_effective = -1188.56° could not be interpolated
Span position -12.41 mm, Re = 89511, AoA_effective = -1094.85° could not be interpolated
Span position -2.51 mm, Re = 90866, AoA_effective = -1046.78° could not be interpolated
Span position 2.51 mm, Re = 90866, AoA_effective = -1046.81° could not be interpolated
Span position 12.41 mm, Re = 89511, AoA_effective = -1095.05° could not be interpolated
Span position 31.72 mm, Re = 86869, AoA_effective = -1188.76° could not be interpolated
Span position 59.47 mm, Re = 83073, AoA_effective = -1316.48° could not be interpolated
Span position 94.26 mm, Re = 78312, AoA_effective = -1438.21° could not be interpolated
Span position 134.36 mm, Re = 72827, AoA_effective = -1461.83° could not be interpolated
Span position 177.75 mm, Re = 66890, AoA_effective = -1047.26° could not be interpolated
Calculating Fin
Interpolating viscous properties …
Computing Plane for alpha=-1.50° beta=0.00°
Calculating aerodynamic coefficients…
Calculating Main Wing
Interpolating viscous properties …
Span position -190.05 mm, Re = 96611, AoA_effective = 660.76° could not be interpolated
Span position -149.48 mm, Re = 99019, AoA_effective = 1337.18° could not be interpolated
Span position -113.34 mm, Re = 101163, AoA_effective = 1490.04° could not be interpolated
Span position -81.90 mm, Re = 103029, AoA_effective = 1478.92° could not be interpolated
Span position -55.36 mm, Re = 104604, AoA_effective = 1421.62° could not be interpolated
Span position -33.91 mm, Re = 105877, AoA_effective = 1352.78° could not be interpolated
Span position -17.70 mm, Re = 106839, AoA_effective = 1294.58° could not be interpolated
Span position -6.82 mm, Re = 107484, AoA_effective = 1257.29° could not be interpolated
Span position -1.37 mm, Re = 107808, AoA_effective = 1241.70° could not be interpolated
Span position 1.37 mm, Re = 107808, AoA_effective = 1241.73° could not be interpolated
Span position 6.82 mm, Re = 107484, AoA_effective = 1257.35° could not be interpolated
Span position 17.70 mm, Re = 106839, AoA_effective = 1294.70° could not be interpolated
Span position 33.91 mm, Re = 105877, AoA_effective = 1352.90° could not be interpolated
Span position 55.36 mm, Re = 104604, AoA_effective = 1421.72° could not be interpolated
Span position 81.90 mm, Re = 103029, AoA_effective = 1478.95° could not be interpolated
Span position 113.34 mm, Re = 101163, AoA_effective = 1490.02° could not be interpolated
Span position 149.48 mm, Re = 99019, AoA_effective = 1336.86° could not be interpolated
Span position 190.05 mm, Re = 96611, AoA_effective = 660.22° could not be interpolated
Calculating Elevator
Interpolating viscous properties …
Span position -177.75 mm, Re = 63299, AoA_effective = -1334.55° could not be interpolated
Span position -134.36 mm, Re = 68916, AoA_effective = -1864.71° could not be interpolated
Span position -94.26 mm, Re = 74107, AoA_effective = -1836.62° could not be interpolated
Span position -59.47 mm, Re = 78612, AoA_effective = -1682.88° could not be interpolated
Span position -31.72 mm, Re = 82204, AoA_effective = -1520.94° could not be interpolated
Span position -12.41 mm, Re = 84704, AoA_effective = -1402.07° could not be interpolated
Span position -2.51 mm, Re = 85987, AoA_effective = -1341.12° could not be interpolated
Span position 2.51 mm, Re = 85987, AoA_effective = -1341.17° could not be interpolated
Span position 12.41 mm, Re = 84704, AoA_effective = -1402.33° could not be interpolated
Span position 31.72 mm, Re = 82204, AoA_effective = -1521.20° could not be interpolated
Span position 59.47 mm, Re = 78612, AoA_effective = -1683.07° could not be interpolated
Span position 94.26 mm, Re = 74107, AoA_effective = -1836.74° could not be interpolated
Span position 134.36 mm, Re = 68916, AoA_effective = -1864.80° could not be interpolated
Span position 177.75 mm, Re = 63299, AoA_effective = -1334.59° could not be interpolated
Calculating Fin
Interpolating viscous properties …
Computing Plane for alpha=-1.00° beta=0.00°
Calculating aerodynamic coefficients…
Calculating Main Wing
Interpolating viscous properties …
Span position -190.05 mm, Re = 92127, AoA_effective = 811.88° could not be interpolated
Span position -149.48 mm, Re = 94423, AoA_effective = 1642.70° could not be interpolated
Span position -113.34 mm, Re = 96468, AoA_effective = 1830.29° could not be interpolated
Span position -81.90 mm, Re = 98247, AoA_effective = 1816.48° could not be interpolated
Span position -55.36 mm, Re = 99748, AoA_effective = 1746.02° could not be interpolated
Span position -33.91 mm, Re = 100962, AoA_effective = 1661.42° could not be interpolated
Span position -17.70 mm, Re = 101880, AoA_effective = 1589.93° could not be interpolated
Span position -6.82 mm, Re = 102495, AoA_effective = 1544.12° could not be interpolated
Span position -1.37 mm, Re = 102804, AoA_effective = 1524.98° could not be interpolated
Span position 1.37 mm, Re = 102804, AoA_effective = 1525.01° could not be interpolated
Span position 6.82 mm, Re = 102495, AoA_effective = 1544.19° could not be interpolated
Span position 17.70 mm, Re = 101880, AoA_effective = 1590.07° could not be interpolated
Span position 33.91 mm, Re = 100962, AoA_effective = 1661.57° could not be interpolated
Span position 55.36 mm, Re = 99748, AoA_effective = 1746.14° could not be interpolated
Span position 81.90 mm, Re = 98247, AoA_effective = 1816.52° could not be interpolated
Span position 113.34 mm, Re = 96468, AoA_effective = 1830.26° could not be interpolated
Span position 149.48 mm, Re = 94423, AoA_effective = 1642.30° could not be interpolated
Span position 190.05 mm, Re = 92127, AoA_effective = 811.22° could not be interpolated
Calculating Elevator
Interpolating viscous properties …
Span position -177.75 mm, Re = 60361, AoA_effective = -1656.35° could not be interpolated
Span position -134.36 mm, Re = 65717, AoA_effective = -2316.21° could not be interpolated
Span position -94.26 mm, Re = 70668, AoA_effective = -2283.34° could not be interpolated
Span position -59.47 mm, Re = 74963, AoA_effective = -2093.95° could not be interpolated
Span position -31.72 mm, Re = 78389, AoA_effective = -1893.84° could not be interpolated
Span position -12.41 mm, Re = 80773, AoA_effective = -1746.85° could not be interpolated
Span position -2.51 mm, Re = 81995, AoA_effective = -1671.49° could not be interpolated
Span position 2.51 mm, Re = 81995, AoA_effective = -1671.55° could not be interpolated
Span position 12.41 mm, Re = 80773, AoA_effective = -1747.16° could not be interpolated
Span position 31.72 mm, Re = 78389, AoA_effective = -1894.16° could not be interpolated
Span position 59.47 mm, Re = 74963, AoA_effective = -2094.18° could not be interpolated
Span position 94.26 mm, Re = 70668, AoA_effective = -2283.48° could not be interpolated
Span position 134.36 mm, Re = 65717, AoA_effective = -2316.32° could not be interpolated
Span position 177.75 mm, Re = 60361, AoA_effective = -1656.40° could not be interpolated
Calculating Fin
Interpolating viscous properties …
Computing Plane for alpha=-0.50° beta=0.00°
Calculating aerodynamic coefficients…
Calculating Main Wing
Interpolating viscous properties …
Span position -190.05 mm, Re = 88431, AoA_effective = 978.31° could not be interpolated
Span position -149.48 mm, Re = 90635, AoA_effective = 1979.22° could not be interpolated
Span position -113.34 mm, Re = 92597, AoA_effective = 2205.07° could not be interpolated
Span position -81.90 mm, Re = 94305, AoA_effective = 2188.30° could not be interpolated
Span position -55.36 mm, Re = 95746, AoA_effective = 2103.33° could not be interpolated
Span position -33.91 mm, Re = 96911, AoA_effective = 2001.37° could not be interpolated
Span position -17.70 mm, Re = 97792, AoA_effective = 1915.23° could not be interpolated
Span position -6.82 mm, Re = 98383, AoA_effective = 1860.03° could not be interpolated
Span position -1.37 mm, Re = 98679, AoA_effective = 1836.97° could not be interpolated
Span position 1.37 mm, Re = 98679, AoA_effective = 1837.01° could not be interpolated
Span position 6.82 mm, Re = 98383, AoA_effective = 1860.12° could not be interpolated
Span position 17.70 mm, Re = 97792, AoA_effective = 1915.39° could not be interpolated
Span position 33.91 mm, Re = 96911, AoA_effective = 2001.55° could not be interpolated
Span position 55.36 mm, Re = 95746, AoA_effective = 2103.48° could not be interpolated
Span position 81.90 mm, Re = 94305, AoA_effective = 2188.34° could not be interpolated
Span position 113.34 mm, Re = 92597, AoA_effective = 2205.03° could not be interpolated
Span position 149.48 mm, Re = 90635, AoA_effective = 1978.74° could not be interpolated
Span position 190.05 mm, Re = 88431, AoA_effective = 977.51° could not be interpolated
Calculating Elevator
Interpolating viscous properties …
Span position -177.75 mm, Re = 57939, AoA_effective = -2012.55° could not be interpolated
Span position -134.36 mm, Re = 63081, AoA_effective = -2816.13° could not be interpolated
Span position -94.26 mm, Re = 67832, AoA_effective = -2778.13° could not be interpolated
Span position -59.47 mm, Re = 71955, AoA_effective = -2549.42° could not be interpolated
Span position -31.72 mm, Re = 75244, AoA_effective = -2307.13° could not be interpolated
Span position -12.41 mm, Re = 77532, AoA_effective = -2129.06° could not be interpolated
Span position -2.51 mm, Re = 78706, AoA_effective = -2037.80° could not be interpolated
Span position 2.51 mm, Re = 78706, AoA_effective = -2037.87° could not be interpolated
Span position 12.41 mm, Re = 77532, AoA_effective = -2129.45° could not be interpolated
Span position 31.72 mm, Re = 75244, AoA_effective = -2307.52° could not be interpolated
Span position 59.47 mm, Re = 71955, AoA_effective = -2549.70° could not be interpolated
Span position 94.26 mm, Re = 67832, AoA_effective = -2778.30° could not be interpolated
Span position 134.36 mm, Re = 63081, AoA_effective = -2816.26° could not be interpolated
Span position 177.75 mm, Re = 57939, AoA_effective = -2012.61° could not be interpolated
Calculating Fin
Interpolating viscous properties …
Computing Plane for alpha=0.00° beta=0.00°
Calculating aerodynamic coefficients…
Calculating Main Wing
Interpolating viscous properties …
Span position -190.05 mm, Re = 85376, AoA_effective = 1160.00° could not be interpolated
Span position -149.48 mm, Re = 87504, AoA_effective = 2346.68° could not be interpolated
Span position -113.34 mm, Re = 89399, AoA_effective = 2614.27° could not be interpolated
Span position -81.90 mm, Re = 91048, AoA_effective = 2594.26° could not be interpolated
Span position -55.36 mm, Re = 92439, AoA_effective = 2493.44° could not be interpolated
Span position -33.91 mm, Re = 93564, AoA_effective = 2372.51° could not be interpolated
Span position -17.70 mm, Re = 94414, AoA_effective = 2270.37° could not be interpolated
Span position -6.82 mm, Re = 94985, AoA_effective = 2204.93° could not be interpolated
Span position -1.37 mm, Re = 95271, AoA_effective = 2177.58° could not be interpolated
Span position 1.37 mm, Re = 95271, AoA_effective = 2177.63° could not be interpolated
Span position 6.82 mm, Re = 94985, AoA_effective = 2205.03° could not be interpolated
Span position 17.70 mm, Re = 94414, AoA_effective = 2270.56° could not be interpolated
Span position 33.91 mm, Re = 93564, AoA_effective = 2372.73° could not be interpolated
Span position 55.36 mm, Re = 92439, AoA_effective = 2493.61° could not be interpolated
Span position 81.90 mm, Re = 91048, AoA_effective = 2594.30° could not be interpolated
Span position 113.34 mm, Re = 89399, AoA_effective = 2614.23° could not be interpolated
Span position 149.48 mm, Re = 87504, AoA_effective = 2346.10° could not be interpolated
Span position 190.05 mm, Re = 85376, AoA_effective = 1159.05° could not be interpolated
Calculating Elevator
Interpolating viscous properties …
Span position -177.75 mm, Re = 55938, AoA_effective = -2403.03° could not be interpolated
Span position -134.36 mm, Re = 60902, AoA_effective = -3364.31° could not be interpolated
Span position -94.26 mm, Re = 65489, AoA_effective = -3320.86° could not be interpolated
Span position -59.47 mm, Re = 69470, AoA_effective = -3049.15° could not be interpolated
Span position -31.72 mm, Re = 72645, AoA_effective = -2760.70° could not be interpolated
Span position -12.41 mm, Re = 74854, AoA_effective = -2548.61° could not be interpolated
Span position -2.51 mm, Re = 75987, AoA_effective = -2439.93° could not be interpolated
Span position 2.51 mm, Re = 75987, AoA_effective = -2440.01° could not be interpolated
Span position 12.41 mm, Re = 74854, AoA_effective = -2549.06° could not be interpolated
Span position 31.72 mm, Re = 72645, AoA_effective = -2761.16° could not be interpolated
Span position 59.47 mm, Re = 69470, AoA_effective = -3049.48° could not be interpolated
Span position 94.26 mm, Re = 65489, AoA_effective = -3321.06° could not be interpolated
Span position 134.36 mm, Re = 60902, AoA_effective = -3364.46° could not be interpolated
Span position 177.75 mm, Re = 55938, AoA_effective = -2403.10° could not be interpolated
Calculating Fin
Interpolating viscous properties …
Computing Plane for alpha=0.50° beta=0.00°
Calculating aerodynamic coefficients…
Calculating Main Wing
Interpolating viscous properties …
Span position -190.05 mm, Re = 82860, AoA_effective = 1356.88° could not be interpolated
Span position -149.48 mm, Re = 84925, AoA_effective = 2744.93° could not be interpolated
Span position -113.34 mm, Re = 86764, AoA_effective = 3057.79° could not be interpolated
Span position -81.90 mm, Re = 88365, AoA_effective = 3034.23° could not be interpolated
Span position -55.36 mm, Re = 89715, AoA_effective = 2916.22° could not be interpolated
Span position -33.91 mm, Re = 90807, AoA_effective = 2774.74° could not be interpolated
Span position -17.70 mm, Re = 91632, AoA_effective = 2655.24° could not be interpolated
Span position -6.82 mm, Re = 92186, AoA_effective = 2578.69° could not be interpolated
Span position -1.37 mm, Re = 92463, AoA_effective = 2546.71° could not be interpolated
Span position 1.37 mm, Re = 92463, AoA_effective = 2546.76° could not be interpolated
Span position 6.82 mm, Re = 92186, AoA_effective = 2578.81° could not be interpolated
Span position 17.70 mm, Re = 91632, AoA_effective = 2655.47° could not be interpolated
Span position 33.91 mm, Re = 90807, AoA_effective = 2774.98° could not be interpolated
Span position 55.36 mm, Re = 89715, AoA_effective = 2916.42° could not be interpolated
Span position 81.90 mm, Re = 88365, AoA_effective = 3034.29° could not be interpolated
Span position 113.34 mm, Re = 86764, AoA_effective = 3057.74° could not be interpolated
Span position 149.48 mm, Re = 84925, AoA_effective = 2744.26° could not be interpolated
Span position 190.05 mm, Re = 82860, AoA_effective = 1355.77° could not be interpolated
Calculating Elevator
Interpolating viscous properties …
Span position -177.75 mm, Re = 54289, AoA_effective = -2827.67° could not be interpolated
Span position -134.36 mm, Re = 59107, AoA_effective = -3960.59° could not be interpolated
Span position -94.26 mm, Re = 63559, AoA_effective = -3911.34° could not be interpolated
Span position -59.47 mm, Re = 67423, AoA_effective = -3592.99° could not be interpolated
Span position -31.72 mm, Re = 70504, AoA_effective = -3254.40° could not be interpolated
Span position -12.41 mm, Re = 72648, AoA_effective = -3005.35° could not be interpolated
Span position -2.51 mm, Re = 73748, AoA_effective = -2877.75° could not be interpolated
Span position 2.51 mm, Re = 73748, AoA_effective = -2877.85° could not be interpolated
Span position 12.41 mm, Re = 72648, AoA_effective = -3005.88° could not be interpolated
Span position 31.72 mm, Re = 70504, AoA_effective = -3254.95° could not be interpolated
Span position 59.47 mm, Re = 67423, AoA_effective = -3593.38° could not be interpolated
Span position 94.26 mm, Re = 63559, AoA_effective = -3911.58° could not be interpolated
Span position 134.36 mm, Re = 59107, AoA_effective = -3960.76° could not be interpolated
Span position 177.75 mm, Re = 54289, AoA_effective = -2827.76° could not be interpolated
Calculating Fin
Interpolating viscous properties …
Computing Plane for alpha=1.00° beta=0.00°
Calculating aerodynamic coefficients…
Calculating Main Wing
Interpolating viscous properties …
Span position -190.05 mm, Re = 80809, AoA_effective = 1568.89° could not be interpolated
Span position -149.48 mm, Re = 82823, AoA_effective = 3173.86° could not be interpolated
Span position -113.34 mm, Re = 84616, AoA_effective = 3535.47° could not be interpolated
Span position -81.90 mm, Re = 86177, AoA_effective = 3508.09° could not be interpolated
Span position -55.36 mm, Re = 87494, AoA_effective = 3371.56° could not be interpolated
Span position -33.91 mm, Re = 88559, AoA_effective = 3207.92° could not be interpolated
Span position -17.70 mm, Re = 89364, AoA_effective = 3069.73° could not be interpolated
Span position -6.82 mm, Re = 89903, AoA_effective = 2981.21° could not be interpolated
Span position -1.37 mm, Re = 90174, AoA_effective = 2944.23° could not be interpolated
Span position 1.37 mm, Re = 90174, AoA_effective = 2944.30° could not be interpolated
Span position 6.82 mm, Re = 89903, AoA_effective = 2981.35° could not be interpolated
Span position 17.70 mm, Re = 89364, AoA_effective = 3070.00° could not be interpolated
Span position 33.91 mm, Re = 88559, AoA_effective = 3208.21° could not be interpolated
Span position 55.36 mm, Re = 87494, AoA_effective = 3371.79° could not be interpolated
Span position 81.90 mm, Re = 86177, AoA_effective = 3508.15° could not be interpolated
Span position 113.34 mm, Re = 84616, AoA_effective = 3535.41° could not be interpolated
Span position 149.48 mm, Re = 82823, AoA_effective = 3173.09° could not be interpolated
Span position 190.05 mm, Re = 80809, AoA_effective = 1567.60° could not be interpolated
Calculating Elevator
Interpolating viscous properties …
Span position -177.75 mm, Re = 52945, AoA_effective = -3286.35° could not be interpolated
Span position -134.36 mm, Re = 57644, AoA_effective = -4604.77° could not be interpolated
Span position -94.26 mm, Re = 61986, AoA_effective = -4549.42° could not be interpolated
Span position -59.47 mm, Re = 65754, AoA_effective = -4180.77° could not be interpolated
Span position -31.72 mm, Re = 68759, AoA_effective = -3788.09° could not be interpolated
Span position -12.41 mm, Re = 70850, AoA_effective = -3499.15° could not be interpolated
Span position -2.51 mm, Re = 71922, AoA_effective = -3351.14° could not be interpolated
Span position 2.51 mm, Re = 71922, AoA_effective = -3351.26° could not be interpolated
Span position 12.41 mm, Re = 70850, AoA_effective = -3499.77° could not be interpolated
Span position 31.72 mm, Re = 68759, AoA_effective = -3788.72° could not be interpolated
Span position 59.47 mm, Re = 65754, AoA_effective = -4181.22° could not be interpolated
Span position 94.26 mm, Re = 61986, AoA_effective = -4549.69° could not be interpolated
Span position 134.36 mm, Re = 57644, AoA_effective = -4604.98° could not be interpolated
Span position 177.75 mm, Re = 52945, AoA_effective = -3286.45° could not be interpolated
Calculating Fin
Interpolating viscous properties …
Computing Plane for alpha=1.50° beta=0.00°
Calculating aerodynamic coefficients…
Calculating Main Wing
Interpolating viscous properties …
Span position -190.05 mm, Re = 79170, AoA_effective = 1795.98° could not be interpolated
Span position -149.48 mm, Re = 81143, AoA_effective = 3633.34° could not be interpolated
Span position -113.34 mm, Re = 82900, AoA_effective = 4047.16° could not be interpolated
Span position -81.90 mm, Re = 84429, AoA_effective = 4015.69° could not be interpolated
Span position -55.36 mm, Re = 85719, AoA_effective = 3859.30° could not be interpolated
Span position -33.91 mm, Re = 86762, AoA_effective = 3671.94° could not be interpolated
Span position -17.70 mm, Re = 87551, AoA_effective = 3513.73° could not be interpolated
Span position -6.82 mm, Re = 88080, AoA_effective = 3412.38° could not be interpolated
Span position -1.37 mm, Re = 88345, AoA_effective = 3370.05° could not be interpolated
Span position 1.37 mm, Re = 88345, AoA_effective = 3370.12° could not be interpolated
Span position 6.82 mm, Re = 88080, AoA_effective = 3412.54° could not be interpolated
Span position 17.70 mm, Re = 87551, AoA_effective = 3514.03° could not be interpolated
Span position 33.91 mm, Re = 86762, AoA_effective = 3672.27° could not be interpolated
Span position 55.36 mm, Re = 85719, AoA_effective = 3859.57° could not be interpolated
Span position 81.90 mm, Re = 84429, AoA_effective = 4015.76° could not be interpolated
Span position 113.34 mm, Re = 82900, AoA_effective = 4047.09° could not be interpolated
Span position 149.48 mm, Re = 81143, AoA_effective = 3632.45° could not be interpolated
Span position 190.05 mm, Re = 79170, AoA_effective = 1794.50° could not be interpolated
Calculating Elevator
Interpolating viscous properties …
Span position -177.75 mm, Re = 51871, AoA_effective = -3778.92° could not be interpolated
Span position -134.36 mm, Re = 56474, AoA_effective = -5296.68° could not be interpolated
Span position -94.26 mm, Re = 60729, AoA_effective = -5234.88° could not be interpolated
Span position -59.47 mm, Re = 64420, AoA_effective = -4812.31° could not be interpolated
Span position -31.72 mm, Re = 67364, AoA_effective = -4361.60° could not be interpolated
Span position -12.41 mm, Re = 69413, AoA_effective = -4029.87° could not be interpolated
Span position -2.51 mm, Re = 70463, AoA_effective = -3859.95° could not be interpolated
Span position 2.51 mm, Re = 70463, AoA_effective = -3860.09° could not be interpolated
Span position 12.41 mm, Re = 69413, AoA_effective = -4030.58° could not be interpolated
Span position 31.72 mm, Re = 67364, AoA_effective = -4362.32° could not be interpolated
Span position 59.47 mm, Re = 64420, AoA_effective = -4812.83° could not be interpolated
Span position 94.26 mm, Re = 60729, AoA_effective = -5235.19° could not be interpolated
Span position 134.36 mm, Re = 56474, AoA_effective = -5296.92° could not be interpolated
Span position 177.75 mm, Re = 51871, AoA_effective = -3779.04° could not be interpolated
Calculating Fin
Interpolating viscous properties …
Computing Plane for alpha=2.00° beta=0.00°
Calculating aerodynamic coefficients…
Calculating Main Wing
Interpolating viscous properties …
Span position -190.05 mm, Re = 77907, AoA_effective = 2038.07° could not be interpolated
Span position -149.48 mm, Re = 79849, AoA_effective = 4123.23° could not be interpolated
Span position -113.34 mm, Re = 81578, AoA_effective = 4592.71° could not be interpolated
Span position -81.90 mm, Re = 83082, AoA_effective = 4556.86° could not be interpolated
Span position -55.36 mm, Re = 84352, AoA_effective = 4379.31° could not be interpolated
Span position -33.91 mm, Re = 85378, AoA_effective = 4166.63° could not be interpolated
Span position -17.70 mm, Re = 86155, AoA_effective = 3987.07° could not be interpolated
Span position -6.82 mm, Re = 86675, AoA_effective = 3872.05° could not be interpolated
Span position -1.37 mm, Re = 86936, AoA_effective = 3824.01° could not be interpolated
Span position 1.37 mm, Re = 86936, AoA_effective = 3824.10° could not be interpolated
Span position 6.82 mm, Re = 86675, AoA_effective = 3872.23° could not be interpolated
Span position 17.70 mm, Re = 86155, AoA_effective = 3987.41° could not be interpolated
Span position 33.91 mm, Re = 85378, AoA_effective = 4167.01° could not be interpolated
Span position 55.36 mm, Re = 84352, AoA_effective = 4379.61° could not be interpolated
Span position 81.90 mm, Re = 83082, AoA_effective = 4556.94° could not be interpolated
Span position 113.34 mm, Re = 81578, AoA_effective = 4592.63° could not be interpolated
Span position 149.48 mm, Re = 79849, AoA_effective = 4122.22° could not be interpolated
Span position 190.05 mm, Re = 77907, AoA_effective = 2036.40° could not be interpolated
Calculating Elevator
Interpolating viscous properties …
Span position -177.75 mm, Re = 51044, AoA_effective = -4305.24° could not be interpolated
Span position -134.36 mm, Re = 55574, AoA_effective = -6036.09° could not be interpolated
Span position -94.26 mm, Re = 59760, AoA_effective = -5967.52° could not be interpolated
Span position -59.47 mm, Re = 63392, AoA_effective = -5487.42° could not be interpolated
Span position -31.72 mm, Re = 66289, AoA_effective = -4974.76° could not be interpolated
Span position -12.41 mm, Re = 68305, AoA_effective = -4597.33° could not be interpolated
Span position -2.51 mm, Re = 69339, AoA_effective = -4404.03° could not be interpolated
Span position 2.51 mm, Re = 69339, AoA_effective = -4404.18° could not be interpolated
Span position 12.41 mm, Re = 68305, AoA_effective = -4598.13° could not be interpolated
Span position 31.72 mm, Re = 66289, AoA_effective = -4975.58° could not be interpolated
Span position 59.47 mm, Re = 63392, AoA_effective = -5488.02° could not be interpolated
Span position 94.26 mm, Re = 59760, AoA_effective = -5967.88° could not be interpolated
Span position 134.36 mm, Re = 55574, AoA_effective = -6036.36° could not be interpolated
Span position 177.75 mm, Re = 51044, AoA_effective = -4305.37° could not be interpolated
Calculating Fin
Interpolating viscous properties …
Computing Plane for alpha=2.50° beta=0.00°
Calculating aerodynamic coefficients…
Calculating Main Wing
Interpolating viscous properties …
Span position -190.05 mm, Re = 76999, AoA_effective = 2295.09° could not be interpolated
Span position -149.48 mm, Re = 78918, AoA_effective = 4643.39° could not be interpolated
Span position -113.34 mm, Re = 80626, AoA_effective = 5171.95° could not be interpolated
Span position -81.90 mm, Re = 82113, AoA_effective = 5131.45° could not be interpolated
Span position -55.36 mm, Re = 83368, AoA_effective = 4931.41° could not be interpolated
Span position -33.91 mm, Re = 84383, AoA_effective = 4691.86° could not be interpolated
Span position -17.70 mm, Re = 85150, AoA_effective = 4489.62° could not be interpolated
Span position -6.82 mm, Re = 85664, AoA_effective = 4360.09° could not be interpolated
Span position -1.37 mm, Re = 85922, AoA_effective = 4305.99° could not be interpolated
Span position 1.37 mm, Re = 85922, AoA_effective = 4306.08° could not be interpolated
Span position 6.82 mm, Re = 85664, AoA_effective = 4360.29° could not be interpolated
Span position 17.70 mm, Re = 85150, AoA_effective = 4490.01° could not be interpolated
Span position 33.91 mm, Re = 84383, AoA_effective = 4692.28° could not be interpolated
Span position 55.36 mm, Re = 83368, AoA_effective = 4931.76° could not be interpolated
Span position 81.90 mm, Re = 82113, AoA_effective = 5131.54° could not be interpolated
Span position 113.34 mm, Re = 80626, AoA_effective = 5171.86° could not be interpolated
Span position 149.48 mm, Re = 78918, AoA_effective = 4642.25° could not be interpolated
Span position 190.05 mm, Re = 76999, AoA_effective = 2293.20° could not be interpolated
Calculating Elevator
Interpolating viscous properties …
Span position -177.75 mm, Re = 50449, AoA_effective = -4865.14° could not be interpolated
Span position -134.36 mm, Re = 54926, AoA_effective = -6822.79° could not be interpolated
Span position -94.26 mm, Re = 59063, AoA_effective = -6747.12° could not be interpolated
Span position -59.47 mm, Re = 62653, AoA_effective = -6205.90° could not be interpolated
Span position -31.72 mm, Re = 65516, AoA_effective = -5627.38° could not be interpolated
Span position -12.41 mm, Re = 67509, AoA_effective = -5201.36° could not be interpolated
Span position -2.51 mm, Re = 68531, AoA_effective = -4983.20° could not be interpolated
Span position 2.51 mm, Re = 68531, AoA_effective = -4983.37° could not be interpolated
Span position 12.41 mm, Re = 67509, AoA_effective = -5202.27° could not be interpolated
Span position 31.72 mm, Re = 65516, AoA_effective = -5628.31° could not be interpolated
Span position 59.47 mm, Re = 62653, AoA_effective = -6206.57° could not be interpolated
Span position 94.26 mm, Re = 59063, AoA_effective = -6747.53° could not be interpolated
Span position 134.36 mm, Re = 54926, AoA_effective = -6823.09° could not be interpolated
Span position 177.75 mm, Re = 50449, AoA_effective = -4865.29° could not be interpolated
Calculating Fin
Interpolating viscous properties …
Computing Plane for alpha=3.00° beta=0.00°
Calculating aerodynamic coefficients…
Calculating Main Wing
Interpolating viscous properties …
Span position -190.05 mm, Re = 76435, AoA_effective = 2566.95° could not be interpolated
Span position -149.48 mm, Re = 78340, AoA_effective = 5193.65° could not be interpolated
Span position -113.34 mm, Re = 80036, AoA_effective = 5784.71° could not be interpolated
Span position -81.90 mm, Re = 81512, AoA_effective = 5739.28° could not be interpolated
Span position -55.36 mm, Re = 82758, AoA_effective = 5515.45° could not be interpolated
Span position -33.91 mm, Re = 83765, AoA_effective = 5247.46° could not be interpolated
Span position -17.70 mm, Re = 84526, AoA_effective = 5021.23° could not be interpolated
Span position -6.82 mm, Re = 85037, AoA_effective = 4876.34° could not be interpolated
Span position -1.37 mm, Re = 85293, AoA_effective = 4815.82° could not be interpolated
Span position 1.37 mm, Re = 85293, AoA_effective = 4815.93° could not be interpolated
Span position 6.82 mm, Re = 85037, AoA_effective = 4876.56° could not be interpolated
Span position 17.70 mm, Re = 84526, AoA_effective = 5021.67° could not be interpolated
Span position 33.91 mm, Re = 83765, AoA_effective = 5247.93° could not be interpolated
Span position 55.36 mm, Re = 82758, AoA_effective = 5515.83° could not be interpolated
Span position 81.90 mm, Re = 81512, AoA_effective = 5739.38° could not be interpolated
Span position 113.34 mm, Re = 80036, AoA_effective = 5784.62° could not be interpolated
Span position 149.48 mm, Re = 78340, AoA_effective = 5192.38° could not be interpolated
Span position 190.05 mm, Re = 76435, AoA_effective = 2564.84° could not be interpolated
Calculating Elevator
Interpolating viscous properties …
Span position -177.75 mm, Re = 50079, AoA_effective = -5458.46° could not be interpolated
Span position -134.36 mm, Re = 54523, AoA_effective = -7656.52° could not be interpolated
Span position -94.26 mm, Re = 58631, AoA_effective = -7573.43° could not be interpolated
Span position -59.47 mm, Re = 62195, AoA_effective = -6967.53° could not be interpolated
Span position -31.72 mm, Re = 65037, AoA_effective = -6319.26° could not be interpolated
Span position -12.41 mm, Re = 67015, AoA_effective = -5841.79° could not be interpolated
Span position -2.51 mm, Re = 68029, AoA_effective = -5597.30° could not be interpolated
Span position 2.51 mm, Re = 68029, AoA_effective = -5597.49° could not be interpolated
Span position 12.41 mm, Re = 67015, AoA_effective = -5842.81° could not be interpolated
Span position 31.72 mm, Re = 65037, AoA_effective = -6320.30° could not be interpolated
Span position 59.47 mm, Re = 62195, AoA_effective = -6968.28° could not be interpolated
Span position 94.26 mm, Re = 58631, AoA_effective = -7573.89° could not be interpolated
Span position 134.36 mm, Re = 54523, AoA_effective = -7656.86° could not be interpolated
Span position 177.75 mm, Re = 50079, AoA_effective = -5458.62° could not be interpolated
Calculating Fin
Interpolating viscous properties …
Computing Plane for alpha=3.50° beta=0.00°
Calculating aerodynamic coefficients…
Calculating Main Wing
Interpolating viscous properties …
Span position -190.05 mm, Re = 76218, AoA_effective = 2853.57° could not be interpolated
Span position -149.48 mm, Re = 78117, AoA_effective = 5773.84° could not be interpolated
Span position -113.34 mm, Re = 79809, AoA_effective = 6430.81° could not be interpolated
Span position -81.90 mm, Re = 81281, AoA_effective = 6380.16° could not be interpolated
Span position -55.36 mm, Re = 82523, AoA_effective = 6131.24° could not be interpolated
Span position -33.91 mm, Re = 83527, AoA_effective = 5833.26° could not be interpolated
Span position -17.70 mm, Re = 84287, AoA_effective = 5581.74° could not be interpolated
Span position -6.82 mm, Re = 84796, AoA_effective = 5420.64° could not be interpolated
Span position -1.37 mm, Re = 85051, AoA_effective = 5353.37° could not be interpolated
Span position 1.37 mm, Re = 85051, AoA_effective = 5353.48° could not be interpolated
Span position 6.82 mm, Re = 84796, AoA_effective = 5420.89° could not be interpolated
Span position 17.70 mm, Re = 84287, AoA_effective = 5582.22° could not be interpolated
Span position 33.91 mm, Re = 83527, AoA_effective = 5833.79° could not be interpolated
Span position 55.36 mm, Re = 82523, AoA_effective = 6131.67° could not be interpolated
Span position 81.90 mm, Re = 81281, AoA_effective = 6380.27° could not be interpolated
Span position 113.34 mm, Re = 79809, AoA_effective = 6430.70° could not be interpolated
Span position 149.48 mm, Re = 78117, AoA_effective = 5772.42° could not be interpolated
Span position 190.05 mm, Re = 76218, AoA_effective = 2851.23° could not be interpolated
Calculating Elevator
Interpolating viscous properties …
Span position -177.75 mm, Re = 49937, AoA_effective = -6085.00° could not be interpolated
Span position -134.36 mm, Re = 54369, AoA_effective = -8537.04° could not be interpolated
Span position -94.26 mm, Re = 58464, AoA_effective = -8446.22° could not be interpolated
Span position -59.47 mm, Re = 62018, AoA_effective = -7772.07° could not be interpolated
Span position -31.72 mm, Re = 64852, AoA_effective = -7050.19° could not be interpolated
Span position -12.41 mm, Re = 66824, AoA_effective = -6518.41° could not be interpolated
Span position -2.51 mm, Re = 67836, AoA_effective = -6246.14° could not be interpolated
Span position 2.51 mm, Re = 67836, AoA_effective = -6246.35° could not be interpolated
Span position 12.41 mm, Re = 66824, AoA_effective = -6519.55° could not be interpolated
Span position 31.72 mm, Re = 64852, AoA_effective = -7051.35° could not be interpolated
Span position 59.47 mm, Re = 62018, AoA_effective = -7772.90° could not be interpolated
Span position 94.26 mm, Re = 58464, AoA_effective = -8446.73° could not be interpolated
Span position 134.36 mm, Re = 54369, AoA_effective = -8537.43° could not be interpolated
Span position 177.75 mm, Re = 49937, AoA_effective = -6085.19° could not be interpolated
Calculating Fin
Interpolating viscous properties …
Computing Plane for alpha=4.00° beta=0.00°
Calculating aerodynamic coefficients…
Calculating Main Wing
Interpolating viscous properties …
Span position -190.05 mm, Re = 76363, AoA_effective = 3154.87° could not be interpolated
Span position -149.48 mm, Re = 78266, AoA_effective = 6383.78° could not be interpolated
Span position -113.34 mm, Re = 79961, AoA_effective = 7110.04° could not be interpolated
Span position -81.90 mm, Re = 81436, AoA_effective = 7053.90° could not be interpolated
Span position -55.36 mm, Re = 82680, AoA_effective = 6778.60° could not be interpolated
Span position -33.91 mm, Re = 83686, AoA_effective = 6449.09° could not be interpolated
Span position -17.70 mm, Re = 84447, AoA_effective = 6170.97° could not be interpolated
Span position -6.82 mm, Re = 84957, AoA_effective = 5992.84° could not be interpolated
Span position -1.37 mm, Re = 85213, AoA_effective = 5918.45° could not be interpolated
Span position 1.37 mm, Re = 85213, AoA_effective = 5918.58° could not be interpolated
Span position 6.82 mm, Re = 84957, AoA_effective = 5993.11° could not be interpolated
Span position 17.70 mm, Re = 84447, AoA_effective = 6171.50° could not be interpolated
Span position 33.91 mm, Re = 83686, AoA_effective = 6449.67° could not be interpolated
Span position 55.36 mm, Re = 82680, AoA_effective = 6779.07° could not be interpolated
Span position 81.90 mm, Re = 81436, AoA_effective = 7054.03° could not be interpolated
Span position 113.34 mm, Re = 79961, AoA_effective = 7109.92° could not be interpolated
Span position 149.48 mm, Re = 78266, AoA_effective = 6382.21° could not be interpolated
Span position 190.05 mm, Re = 76363, AoA_effective = 3152.28° could not be interpolated
Calculating Elevator
Interpolating viscous properties …
Span position -177.75 mm, Re = 50032, AoA_effective = -6744.59° could not be interpolated
Span position -134.36 mm, Re = 54472, AoA_effective = -9464.09° could not be interpolated
Span position -94.26 mm, Re = 58576, AoA_effective = -9365.21° could not be interpolated
Span position -59.47 mm, Re = 62136, AoA_effective = -8619.28° could not be interpolated
Span position -31.72 mm, Re = 64976, AoA_effective = -7819.96° could not be interpolated
Span position -12.41 mm, Re = 66952, AoA_effective = -7231.03° could not be interpolated
Span position -2.51 mm, Re = 67965, AoA_effective = -6929.51° could not be interpolated
Span position 2.51 mm, Re = 67965, AoA_effective = -6929.75° could not be interpolated
Span position 12.41 mm, Re = 66952, AoA_effective = -7232.29° could not be interpolated
Span position 31.72 mm, Re = 64976, AoA_effective = -7821.24° could not be interpolated
Span position 59.47 mm, Re = 62136, AoA_effective = -8620.20° could not be interpolated
Span position 94.26 mm, Re = 58576, AoA_effective = -9365.78° could not be interpolated
Span position 134.36 mm, Re = 54472, AoA_effective = -9464.51° could not be interpolated
Span position 177.75 mm, Re = 50032, AoA_effective = -6744.80° could not be interpolated
Calculating Fin
Interpolating viscous properties …
Computing Plane for alpha=4.50° beta=0.00°
Calculating aerodynamic coefficients…
Calculating Main Wing
Interpolating viscous properties …
Span position -190.05 mm, Re = 76901, AoA_effective = 3470.75° could not be interpolated
Span position -149.48 mm, Re = 78817, AoA_effective = 7023.28° could not be interpolated
Span position -113.34 mm, Re = 80524, AoA_effective = 7822.20° could not be interpolated
Span position -81.90 mm, Re = 82009, AoA_effective = 7760.30° could not be interpolated
Span position -55.36 mm, Re = 83262, AoA_effective = 7457.32° could not be interpolated
Span position -33.91 mm, Re = 84276, AoA_effective = 7094.75° could not be interpolated
Span position -17.70 mm, Re = 85042, AoA_effective = 6788.74° could not be interpolated
Span position -6.82 mm, Re = 85555, AoA_effective = 6592.75° could not be interpolated
Span position -1.37 mm, Re = 85813, AoA_effective = 6510.91° could not be interpolated
Span position 1.37 mm, Re = 85813, AoA_effective = 6511.05° could not be interpolated
Span position 6.82 mm, Re = 85555, AoA_effective = 6593.05° could not be interpolated
Span position 17.70 mm, Re = 85042, AoA_effective = 6789.32° could not be interpolated
Span position 33.91 mm, Re = 84276, AoA_effective = 7095.39° could not be interpolated
Span position 55.36 mm, Re = 83262, AoA_effective = 7457.84° could not be interpolated
Span position 81.90 mm, Re = 82009, AoA_effective = 7760.43° could not be interpolated
Span position 113.34 mm, Re = 80524, AoA_effective = 7822.06° could not be interpolated
Span position 149.48 mm, Re = 78817, AoA_effective = 7021.56° could not be interpolated
Span position 190.05 mm, Re = 76901, AoA_effective = 3467.90° could not be interpolated
Calculating Elevator
Interpolating viscous properties …
Span position -177.75 mm, Re = 50384, AoA_effective = -7437.02° could not be interpolated
Span position -134.36 mm, Re = 54856, AoA_effective = -10437.37° could not be interpolated
Span position -94.26 mm, Re = 58988, AoA_effective = -10330.12° could not be interpolated
Span position -59.47 mm, Re = 62574, AoA_effective = -9508.90° could not be interpolated
Span position -31.72 mm, Re = 65433, AoA_effective = -8628.31° could not be interpolated
Span position -12.41 mm, Re = 67423, AoA_effective = -7979.41° could not be interpolated
Span position -2.51 mm, Re = 68444, AoA_effective = -7647.21° could not be interpolated
Span position 2.51 mm, Re = 68444, AoA_effective = -7647.48° could not be interpolated
Span position 12.41 mm, Re = 67423, AoA_effective = -7980.80° could not be interpolated
Span position 31.72 mm, Re = 65433, AoA_effective = -8629.72° could not be interpolated
Span position 59.47 mm, Re = 62574, AoA_effective = -9509.92° could not be interpolated
Span position 94.26 mm, Re = 58988, AoA_effective = -10330.75° could not be interpolated
Span position 134.36 mm, Re = 54856, AoA_effective = -10437.83° could not be interpolated
Span position 177.75 mm, Re = 50384, AoA_effective = -7437.25° could not be interpolated
Calculating Fin
Interpolating viscous properties …
Computing Plane for alpha=5.00° beta=0.00°
Calculating aerodynamic coefficients…
Calculating Main Wing
Interpolating viscous properties …
Span position -190.05 mm, Re = 77881, AoA_effective = 3801.11° could not be interpolated
Span position -149.48 mm, Re = 79822, AoA_effective = 7692.16° could not be interpolated
Span position -113.34 mm, Re = 81550, AoA_effective = 8567.06° could not be interpolated
Span position -81.90 mm, Re = 83054, AoA_effective = 8499.13° could not be interpolated
Span position -55.36 mm, Re = 84324, AoA_effective = 8167.21° could not be interpolated
Span position -33.91 mm, Re = 85350, AoA_effective = 7770.05° could not be interpolated
Span position -17.70 mm, Re = 86125, AoA_effective = 7434.86° could not be interpolated
Span position -6.82 mm, Re = 86646, AoA_effective = 7220.19° could not be interpolated
Span position -1.37 mm, Re = 86907, AoA_effective = 7130.56° could not be interpolated
Span position 1.37 mm, Re = 86907, AoA_effective = 7130.71° could not be interpolated
Span position 6.82 mm, Re = 86646, AoA_effective = 7220.53° could not be interpolated
Span position 17.70 mm, Re = 86125, AoA_effective = 7435.50° could not be interpolated
Span position 33.91 mm, Re = 85350, AoA_effective = 7770.74° could not be interpolated
Span position 55.36 mm, Re = 84324, AoA_effective = 8167.77° could not be interpolated
Span position 81.90 mm, Re = 83054, AoA_effective = 8499.28° could not be interpolated
Span position 113.34 mm, Re = 81550, AoA_effective = 8566.92° could not be interpolated
Span position 149.48 mm, Re = 79822, AoA_effective = 7690.27° could not be interpolated
Span position 190.05 mm, Re = 77881, AoA_effective = 3797.99° could not be interpolated
Calculating Elevator
Interpolating viscous properties …
Span position -177.75 mm, Re = 51027, AoA_effective = -8162.08° could not be interpolated
Span position -134.36 mm, Re = 55555, AoA_effective = -11456.59° could not be interpolated
Span position -94.26 mm, Re = 59740, AoA_effective = -11340.66° could not be interpolated
Span position -59.47 mm, Re = 63371, AoA_effective = -10440.66° could not be interpolated
Span position -31.72 mm, Re = 66267, AoA_effective = -9475.02° could not be interpolated
Span position -12.41 mm, Re = 68282, AoA_effective = -8763.35° could not be interpolated
Span position -2.51 mm, Re = 69316, AoA_effective = -8399.03° could not be interpolated
Span position 2.51 mm, Re = 69316, AoA_effective = -8399.32° could not be interpolated
Span position 12.41 mm, Re = 68282, AoA_effective = -8764.87° could not be interpolated
Span position 31.72 mm, Re = 66267, AoA_effective = -9476.56° could not be interpolated
Span position 59.47 mm, Re = 63371, AoA_effective = -10441.78° could not be interpolated
Span position 94.26 mm, Re = 59740, AoA_effective = -11341.35° could not be interpolated
Span position 134.36 mm, Re = 55555, AoA_effective = -11457.10° could not be interpolated
Span position 177.75 mm, Re = 51027, AoA_effective = -8162.33° could not be interpolated
Calculating Fin
Interpolating viscous properties …
Computing Plane for alpha=5.50° beta=0.00°
Calculating aerodynamic coefficients…
Calculating Main Wing
Interpolating viscous properties …
Span position -234.80 mm, Re = 77200, AoA_effective = 15.71° could not be interpolated
Span position -190.05 mm, Re = 79381, AoA_effective = 4145.86° could not be interpolated
Span position -149.48 mm, Re = 81359, AoA_effective = 8390.21° could not be interpolated
Span position -113.34 mm, Re = 83121, AoA_effective = 9344.41° could not be interpolated
Span position -81.90 mm, Re = 84654, AoA_effective = 9270.17° could not be interpolated
Span position -55.36 mm, Re = 85948, AoA_effective = 8908.03° could not be interpolated
Span position -33.91 mm, Re = 86994, AoA_effective = 8474.77° could not be interpolated
Span position -17.70 mm, Re = 87785, AoA_effective = 8109.14° could not be interpolated
Span position -6.82 mm, Re = 88315, AoA_effective = 7874.97° could not be interpolated
Span position -1.37 mm, Re = 88581, AoA_effective = 7777.20° could not be interpolated
Span position 1.37 mm, Re = 88581, AoA_effective = 7777.36° could not be interpolated
Span position 6.82 mm, Re = 88315, AoA_effective = 7875.34° could not be interpolated
Span position 17.70 mm, Re = 87785, AoA_effective = 8109.83° could not be interpolated
Span position 33.91 mm, Re = 86994, AoA_effective = 8475.53° could not be interpolated
Span position 55.36 mm, Re = 85948, AoA_effective = 8908.65° could not be interpolated
Span position 81.90 mm, Re = 84654, AoA_effective = 9270.34° could not be interpolated
Span position 113.34 mm, Re = 83121, AoA_effective = 9344.25° could not be interpolated
Span position 149.48 mm, Re = 81359, AoA_effective = 8388.16° could not be interpolated
Span position 190.05 mm, Re = 79381, AoA_effective = 4142.45° could not be interpolated
Span position 234.80 mm, Re = 77200, AoA_effective = 15.71° could not be interpolated
Calculating Elevator
Interpolating viscous properties …
Span position -177.75 mm, Re = 52010, AoA_effective = -8919.55° could not be interpolated
Span position -134.36 mm, Re = 56625, AoA_effective = -12521.44° could not be interpolated
Span position -94.26 mm, Re = 60891, AoA_effective = -12396.52° could not be interpolated
Span position -59.47 mm, Re = 64592, AoA_effective = -11414.28° could not be interpolated
Span position -31.72 mm, Re = 67544, AoA_effective = -10359.81° could not be interpolated
Span position -12.41 mm, Re = 69598, AoA_effective = -9582.58° could not be interpolated
Span position -2.51 mm, Re = 70651, AoA_effective = -9184.73° could not be interpolated
Span position 2.51 mm, Re = 70651, AoA_effective = -9185.04° could not be interpolated
Span position 12.41 mm, Re = 69598, AoA_effective = -9584.24° could not be interpolated
Span position 31.72 mm, Re = 67544, AoA_effective = -10361.50° could not be interpolated
Span position 59.47 mm, Re = 64592, AoA_effective = -11415.50° could not be interpolated
Span position 94.26 mm, Re = 60891, AoA_effective = -12397.27° could not be interpolated
Span position 134.36 mm, Re = 56625, AoA_effective = -12522.00° could not be interpolated
Span position 177.75 mm, Re = 52010, AoA_effective = -8919.82° could not be interpolated
Calculating Fin
Interpolating viscous properties …
Computing Plane for alpha=6.00° beta=0.00°
Calculating aerodynamic coefficients…
Calculating Main Wing
Interpolating viscous properties …
Span position -448.94 mm, Re = 68558, AoA_effective = 15.25° could not be interpolated
Span position -390.84 mm, Re = 71467, AoA_effective = 15.38° could not be interpolated
Span position -335.54 mm, Re = 74236, AoA_effective = 15.26° could not be interpolated
Span position -234.80 mm, Re = 79280, AoA_effective = 16.40° could not be interpolated
Span position -190.05 mm, Re = 81520, AoA_effective = 4504.89° could not be interpolated
Span position -149.48 mm, Re = 83552, AoA_effective = 9117.22° could not be interpolated
Span position -113.34 mm, Re = 85361, AoA_effective = 10153.99° could not be interpolated
Span position -81.90 mm, Re = 86935, AoA_effective = 10073.19° could not be interpolated
Span position -55.36 mm, Re = 88264, AoA_effective = 9679.57° could not be interpolated
Span position -33.91 mm, Re = 89338, AoA_effective = 9208.71° could not be interpolated
Span position -17.70 mm, Re = 90150, AoA_effective = 8811.36° could not be interpolated
Span position -6.82 mm, Re = 90695, AoA_effective = 8556.89° could not be interpolated
Span position -1.37 mm, Re = 90968, AoA_effective = 8450.64° could not be interpolated
Span position 1.37 mm, Re = 90968, AoA_effective = 8450.82° could not be interpolated
Span position 6.82 mm, Re = 90695, AoA_effective = 8557.29° could not be interpolated
Span position 17.70 mm, Re = 90150, AoA_effective = 8812.11° could not be interpolated
Span position 33.91 mm, Re = 89338, AoA_effective = 9209.53° could not be interpolated
Span position 55.36 mm, Re = 88264, AoA_effective = 9680.24° could not be interpolated
Span position 81.90 mm, Re = 86935, AoA_effective = 10073.36° could not be interpolated
Span position 113.34 mm, Re = 85361, AoA_effective = 10153.82° could not be interpolated
Span position 149.48 mm, Re = 83552, AoA_effective = 9114.99° could not be interpolated
Span position 190.05 mm, Re = 81520, AoA_effective = 4501.19° could not be interpolated
Span position 234.80 mm, Re = 79280, AoA_effective = 16.40° could not be interpolated
Span position 335.54 mm, Re = 74236, AoA_effective = 15.26° could not be interpolated
Span position 390.84 mm, Re = 71467, AoA_effective = 15.38° could not be interpolated
Span position 448.94 mm, Re = 68558, AoA_effective = 15.25° could not be interpolated
Calculating Elevator
Interpolating viscous properties …
Span position -177.75 mm, Re = 53411, AoA_effective = -9709.20° could not be interpolated
Span position -134.36 mm, Re = 58151, AoA_effective = -13631.59° could not be interpolated
Span position -94.26 mm, Re = 62531, AoA_effective = -13497.39° could not be interpolated
Span position -59.47 mm, Re = 66333, AoA_effective = -12429.46° could not be interpolated
Span position -31.72 mm, Re = 69364, AoA_effective = -11282.42° could not be interpolated
Span position -12.41 mm, Re = 71473, AoA_effective = -10436.88° could not be interpolated
Span position -2.51 mm, Re = 72555, AoA_effective = -10004.07° could not be interpolated
Span position 2.51 mm, Re = 72555, AoA_effective = -10004.41° could not be interpolated
Span position 12.41 mm, Re = 71473, AoA_effective = -10438.68° could not be interpolated
Span position 31.72 mm, Re = 69364, AoA_effective = -11284.26° could not be interpolated
Span position 59.47 mm, Re = 66333, AoA_effective = -12430.78° could not be interpolated
Span position 94.26 mm, Re = 62531, AoA_effective = -13498.20° could not be interpolated
Span position 134.36 mm, Re = 58151, AoA_effective = -13632.20° could not be interpolated
Span position 177.75 mm, Re = 53411, AoA_effective = -9709.50° could not be interpolated
Calculating Fin
Interpolating viscous properties …
Computing Plane for alpha=6.50° beta=0.00°
Calculating aerodynamic coefficients…
Calculating Main Wing
Interpolating viscous properties …
Span position -509.44 mm, Re = 67909, AoA_effective = 15.45° could not be interpolated
Span position -448.94 mm, Re = 71048, AoA_effective = 15.82° could not be interpolated
Span position -390.84 mm, Re = 74063, AoA_effective = 15.97° could not be interpolated
Span position -335.54 mm, Re = 76933, AoA_effective = 15.82° could not be interpolated
Span position -283.40 mm, Re = 79638, AoA_effective = 15.26° could not be interpolated
Span position -234.80 mm, Re = 82160, AoA_effective = 17.08° could not be interpolated
Span position -190.05 mm, Re = 84482, AoA_effective = 4878.09° could not be interpolated
Span position -149.48 mm, Re = 86587, AoA_effective = 9872.95° could not be interpolated
Span position -113.34 mm, Re = 88462, AoA_effective = 10995.56° could not be interpolated
Span position -81.90 mm, Re = 90094, AoA_effective = 10907.92° could not be interpolated
Span position -55.36 mm, Re = 91471, AoA_effective = 10481.59° could not be interpolated
Span position -33.91 mm, Re = 92584, AoA_effective = 9971.64° could not be interpolated
Span position -17.70 mm, Re = 93425, AoA_effective = 9541.33° could not be interpolated
Span position -6.82 mm, Re = 93990, AoA_effective = 9265.75° could not be interpolated
Span position -1.37 mm, Re = 94273, AoA_effective = 9150.69° could not be interpolated
Span position 1.37 mm, Re = 94273, AoA_effective = 9150.89° could not be interpolated
Span position 6.82 mm, Re = 93990, AoA_effective = 9266.18° could not be interpolated
Span position 17.70 mm, Re = 93425, AoA_effective = 9542.15° could not be interpolated
Span position 33.91 mm, Re = 92584, AoA_effective = 9972.54° could not be interpolated
Span position 55.36 mm, Re = 91471, AoA_effective = 10482.31° could not be interpolated
Span position 81.90 mm, Re = 90094, AoA_effective = 10908.11° could not be interpolated
Span position 113.34 mm, Re = 88462, AoA_effective = 10995.37° could not be interpolated
Span position 149.48 mm, Re = 86587, AoA_effective = 9870.53° could not be interpolated
Span position 190.05 mm, Re = 84482, AoA_effective = 4874.08° could not be interpolated
Span position 234.80 mm, Re = 82160, AoA_effective = 17.07° could not be interpolated
Span position 283.40 mm, Re = 79638, AoA_effective = 15.26° could not be interpolated
Span position 335.54 mm, Re = 76933, AoA_effective = 15.82° could not be interpolated
Span position 390.84 mm, Re = 74063, AoA_effective = 15.97° could not be interpolated
Span position 448.94 mm, Re = 71048, AoA_effective = 15.82° could not be interpolated
Span position 509.44 mm, Re = 67909, AoA_effective = 15.45° could not be interpolated
Calculating Elevator
Interpolating viscous properties …
Span position -177.75 mm, Re = 55352, AoA_effective = -10530.79° could not be interpolated
Span position -134.36 mm, Re = 60264, AoA_effective = -14786.72° could not be interpolated
Span position -94.26 mm, Re = 64803, AoA_effective = -14642.91° could not be interpolated
Span position -59.47 mm, Re = 68742, AoA_effective = -13485.89° could not be interpolated
Span position -31.72 mm, Re = 71884, AoA_effective = -12242.58° could not be interpolated
Span position -12.41 mm, Re = 74070, AoA_effective = -11325.97° could not be interpolated
Span position -2.51 mm, Re = 75191, AoA_effective = -10856.80° could not be interpolated
Span position 2.51 mm, Re = 75191, AoA_effective = -10857.18° could not be interpolated
Span position 12.41 mm, Re = 74070, AoA_effective = -11327.93° could not be interpolated
Span position 31.72 mm, Re = 71884, AoA_effective = -12244.57° could not be interpolated
Span position 59.47 mm, Re = 68742, AoA_effective = -13487.33° could not be interpolated
Span position 94.26 mm, Re = 64803, AoA_effective = -14643.79° could not be interpolated
Span position 134.36 mm, Re = 60264, AoA_effective = -14787.38° could not be interpolated
Span position 177.75 mm, Re = 55352, AoA_effective = -10531.11° could not be interpolated
Calculating Fin
Interpolating viscous properties …
Computing Plane for alpha=7.00° beta=0.00°
Calculating aerodynamic coefficients…
Calculating Main Wing
Interpolating viscous properties …
Span position -571.93 mm, Re = 67790, AoA_effective = 15.27° could not be interpolated
Span position -509.44 mm, Re = 71188, AoA_effective = 15.96° could not be interpolated
Span position -448.94 mm, Re = 74479, AoA_effective = 16.37° could not be interpolated
Span position -390.84 mm, Re = 77640, AoA_effective = 16.51° could not be interpolated
Span position -335.54 mm, Re = 80648, AoA_effective = 16.35° could not be interpolated
Span position -283.40 mm, Re = 83484, AoA_effective = 15.77° could not be interpolated
Span position -234.80 mm, Re = 86127, AoA_effective = 17.72° could not be interpolated
Span position -190.05 mm, Re = 88561, AoA_effective = 5265.33° could not be interpolated
Span position -149.48 mm, Re = 90768, AoA_effective = 10657.18° could not be interpolated
Span position -113.34 mm, Re = 92734, AoA_effective = 11868.87° could not be interpolated
Span position -81.90 mm, Re = 94444, AoA_effective = 11774.14° could not be interpolated
Span position -55.36 mm, Re = 95888, AoA_effective = 11313.85° could not be interpolated
Span position -33.91 mm, Re = 97055, AoA_effective = 10763.33° could not be interpolated
Span position -17.70 mm, Re = 97937, AoA_effective = 10298.80° could not be interpolated
Span position -6.82 mm, Re = 98528, AoA_effective = 10001.32° could not be interpolated
Span position -1.37 mm, Re = 98825, AoA_effective = 9877.11° could not be interpolated
Span position 1.37 mm, Re = 98825, AoA_effective = 9877.32° could not be interpolated
Span position 6.82 mm, Re = 98528, AoA_effective = 10001.78° could not be interpolated
Span position 17.70 mm, Re = 97937, AoA_effective = 10299.68° could not be interpolated
Span position 33.91 mm, Re = 97055, AoA_effective = 10764.30° could not be interpolated
Span position 55.36 mm, Re = 95888, AoA_effective = 11314.63° could not be interpolated
Span position 81.90 mm, Re = 94444, AoA_effective = 11774.35° could not be interpolated
Span position 113.34 mm, Re = 92734, AoA_effective = 11868.67° could not be interpolated
Span position 149.48 mm, Re = 90768, AoA_effective = 10654.57° could not be interpolated
Span position 190.05 mm, Re = 88561, AoA_effective = 5261.00° could not be interpolated
Span position 234.80 mm, Re = 86127, AoA_effective = 17.72° could not be interpolated
Span position 283.40 mm, Re = 83484, AoA_effective = 15.76° could not be interpolated
Span position 335.54 mm, Re = 80648, AoA_effective = 16.35° could not be interpolated
Span position 390.84 mm, Re = 77640, AoA_effective = 16.51° could not be interpolated
Span position 448.94 mm, Re = 74479, AoA_effective = 16.37° could not be interpolated
Span position 509.44 mm, Re = 71188, AoA_effective = 15.96° could not be interpolated
Span position 571.93 mm, Re = 67790, AoA_effective = 15.27° could not be interpolated
Calculating Elevator
Interpolating viscous properties …
Span position -177.75 mm, Re = 58024, AoA_effective = -11384.06° could not be interpolated
Span position -134.36 mm, Re = 63174, AoA_effective = -15986.45° could not be interpolated
Span position -94.26 mm, Re = 67932, AoA_effective = -15832.75° could not be interpolated
Span position -59.47 mm, Re = 72062, AoA_effective = -14583.24° could not be interpolated
Span position -31.72 mm, Re = 75355, AoA_effective = -13239.98° could not be interpolated
Span position -12.41 mm, Re = 77647, AoA_effective = -12249.59° could not be interpolated
Span position -2.51 mm, Re = 78822, AoA_effective = -11742.67° could not be interpolated
Span position 2.51 mm, Re = 78822, AoA_effective = -11743.07° could not be interpolated
Span position 12.41 mm, Re = 77647, AoA_effective = -12251.70° could not be interpolated
Span position 31.72 mm, Re = 75355, AoA_effective = -13242.13° could not be interpolated
Span position 59.47 mm, Re = 72062, AoA_effective = -14584.80° could not be interpolated
Span position 94.26 mm, Re = 67932, AoA_effective = -15833.71° could not be interpolated
Span position 134.36 mm, Re = 63174, AoA_effective = -15987.17° could not be interpolated
Span position 177.75 mm, Re = 58024, AoA_effective = -11384.41° could not be interpolated
Calculating Fin
Interpolating viscous properties …
Computing Plane for alpha=7.50° beta=0.00°
Calculating aerodynamic coefficients…
Calculating Main Wing
Interpolating viscous properties …
Span position -571.93 mm, Re = 72152, AoA_effective = 15.71° could not be interpolated
Span position -509.44 mm, Re = 75770, AoA_effective = 16.44° could not be interpolated
Span position -448.94 mm, Re = 79273, AoA_effective = 16.85° could not be interpolated
Span position -390.84 mm, Re = 82636, AoA_effective = 17.01° could not be interpolated
Span position -335.54 mm, Re = 85838, AoA_effective = 16.85° could not be interpolated
Span position -283.40 mm, Re = 88857, AoA_effective = 16.22° could not be interpolated
Span position -234.80 mm, Re = 91671, AoA_effective = 18.33° could not be interpolated
Span position -190.05 mm, Re = 94261, AoA_effective = 5666.51° could not be interpolated
Span position -149.48 mm, Re = 96610, AoA_effective = 11469.67° could not be interpolated
Span position -113.34 mm, Re = 98702, AoA_effective = 12773.65° could not be interpolated
Span position -81.90 mm, Re = 100523, AoA_effective = 12671.56° could not be interpolated
Span position -55.36 mm, Re = 102059, AoA_effective = 12176.08° could not be interpolated
Span position -33.91 mm, Re = 103301, AoA_effective = 11583.54° could not be interpolated
Span position -17.70 mm, Re = 104240, AoA_effective = 11083.56° could not be interpolated
Span position -6.82 mm, Re = 104869, AoA_effective = 10763.38° could not be interpolated
Span position -1.37 mm, Re = 105185, AoA_effective = 10629.70° could not be interpolated
Span position 1.37 mm, Re = 105185, AoA_effective = 10629.92° could not be interpolated
Span position 6.82 mm, Re = 104869, AoA_effective = 10763.87° could not be interpolated
Span position 17.70 mm, Re = 104240, AoA_effective = 11084.51° could not be interpolated
Span position 33.91 mm, Re = 103301, AoA_effective = 11584.57° could not be interpolated
Span position 55.36 mm, Re = 102059, AoA_effective = 12176.92° could not be interpolated
Span position 81.90 mm, Re = 100523, AoA_effective = 12671.78° could not be interpolated
Span position 113.34 mm, Re = 98702, AoA_effective = 12773.43° could not be interpolated
Span position 149.48 mm, Re = 96610, AoA_effective = 11466.86° could not be interpolated
Span position 190.05 mm, Re = 94261, AoA_effective = 5661.85° could not be interpolated
Span position 234.80 mm, Re = 91671, AoA_effective = 18.33° could not be interpolated
Span position 283.40 mm, Re = 88857, AoA_effective = 16.22° could not be interpolated
Span position 335.54 mm, Re = 85838, AoA_effective = 16.85° could not be interpolated
Span position 390.84 mm, Re = 82636, AoA_effective = 17.01° could not be interpolated
Span position 448.94 mm, Re = 79273, AoA_effective = 16.85° could not be interpolated
Span position 509.44 mm, Re = 75770, AoA_effective = 16.44° could not be interpolated
Span position 571.93 mm, Re = 72152, AoA_effective = 15.71° could not be interpolated
Calculating Elevator
Interpolating viscous properties …
Span position -177.75 mm, Re = 61759, AoA_effective = -12268.77° could not be interpolated
Span position -134.36 mm, Re = 67239, AoA_effective = -17230.44° could not be interpolated
Span position -94.26 mm, Re = 72304, AoA_effective = -17066.54° could not be interpolated
Span position -59.47 mm, Re = 76700, AoA_effective = -15721.20° could not be interpolated
Span position -31.72 mm, Re = 80205, AoA_effective = -14274.32° could not be interpolated
Span position -12.41 mm, Re = 82644, AoA_effective = -13207.45° could not be interpolated
Span position -2.51 mm, Re = 83895, AoA_effective = -12661.41° could not be interpolated
Span position 2.51 mm, Re = 83895, AoA_effective = -12661.84° could not be interpolated
Span position 12.41 mm, Re = 82644, AoA_effective = -13209.72° could not be interpolated
Span position 31.72 mm, Re = 80205, AoA_effective = -14276.64° could not be interpolated
Span position 59.47 mm, Re = 76700, AoA_effective = -15722.87° could not be interpolated
Span position 94.26 mm, Re = 72304, AoA_effective = -17067.57° could not be interpolated
Span position 134.36 mm, Re = 67239, AoA_effective = -17231.22° could not be interpolated
Span position 177.75 mm, Re = 61759, AoA_effective = -12269.14° could not be interpolated
Calculating Fin
Interpolating viscous properties …
Computing Plane for alpha=8.00° beta=0.00°
Calculating aerodynamic coefficients…
Calculating Main Wing
Interpolating viscous properties …
Span position -571.93 mm, Re = 78469, AoA_effective = 16.09° could not be interpolated
Span position -509.44 mm, Re = 82403, AoA_effective = 16.86° could not be interpolated
Span position -448.94 mm, Re = 86213, AoA_effective = 17.32° could not be interpolated
Span position -390.84 mm, Re = 89871, AoA_effective = 17.47° could not be interpolated
Span position -335.54 mm, Re = 93353, AoA_effective = 17.31° could not be interpolated
Span position -283.40 mm, Re = 96636, AoA_effective = 16.64° could not be interpolated
Span position -234.80 mm, Re = 99696, AoA_effective = 18.91° could not be interpolated
Span position -190.05 mm, Re = 102513, AoA_effective = 6081.49° could not be interpolated
Span position -149.48 mm, Re = 105068, AoA_effective = 12310.18° could not be interpolated
Span position -113.34 mm, Re = 107343, AoA_effective = 13709.62° could not be interpolated
Span position -81.90 mm, Re = 109323, AoA_effective = 13599.92° could not be interpolated
Span position -55.36 mm, Re = 110994, AoA_effective = 13068.03° could not be interpolated
Span position -33.91 mm, Re = 112344, AoA_effective = 12432.01° could not be interpolated
Span position -17.70 mm, Re = 113366, AoA_effective = 11895.36° could not be interpolated
Span position -6.82 mm, Re = 114050, AoA_effective = 11551.70° could not be interpolated
Span position -1.37 mm, Re = 114394, AoA_effective = 11408.22° could not be interpolated
Span position 1.37 mm, Re = 114394, AoA_effective = 11408.47° could not be interpolated
Span position 6.82 mm, Re = 114050, AoA_effective = 11552.23° could not be interpolated
Span position 17.70 mm, Re = 113366, AoA_effective = 11896.38° could not be interpolated
Span position 33.91 mm, Re = 112344, AoA_effective = 12433.12° could not be interpolated
Span position 55.36 mm, Re = 110994, AoA_effective = 13068.94° could not be interpolated
Span position 81.90 mm, Re = 109323, AoA_effective = 13600.16° could not be interpolated
Span position 113.34 mm, Re = 107343, AoA_effective = 13709.39° could not be interpolated
Span position 149.48 mm, Re = 105068, AoA_effective = 12307.16° could not be interpolated
Span position 190.05 mm, Re = 102513, AoA_effective = 6076.49° could not be interpolated
Span position 234.80 mm, Re = 99696, AoA_effective = 18.90° could not be interpolated
Span position 283.40 mm, Re = 96636, AoA_effective = 16.64° could not be interpolated
Span position 335.54 mm, Re = 93353, AoA_effective = 17.31° could not be interpolated
Span position 390.84 mm, Re = 89871, AoA_effective = 17.47° could not be interpolated
Span position 448.94 mm, Re = 86213, AoA_effective = 17.31° could not be interpolated
Span position 509.44 mm, Re = 82403, AoA_effective = 16.86° could not be interpolated
Span position 571.93 mm, Re = 78469, AoA_effective = 16.09° could not be interpolated
Calculating Elevator
Interpolating viscous properties …
Span position -177.75 mm, Re = 67166, AoA_effective = -13184.63° could not be interpolated
Span position -134.36 mm, Re = 73126, AoA_effective = -18518.31° could not be interpolated
Span position -94.26 mm, Re = 78634, AoA_effective = -18343.91° could not be interpolated
Span position -59.47 mm, Re = 83414, AoA_effective = -16899.40° could not be interpolated
Span position -31.72 mm, Re = 87226, AoA_effective = -15345.30° could not be interpolated
Span position -12.41 mm, Re = 89879, AoA_effective = -14199.26° could not be interpolated
Span position -2.51 mm, Re = 91239, AoA_effective = -13612.73° could not be interpolated
Span position 2.51 mm, Re = 91239, AoA_effective = -13613.19° could not be interpolated
Span position 12.41 mm, Re = 89879, AoA_effective = -14201.70° could not be interpolated
Span position 31.72 mm, Re = 87226, AoA_effective = -15347.78° could not be interpolated
Span position 59.47 mm, Re = 83414, AoA_effective = -16901.20° could not be interpolated
Span position 94.26 mm, Re = 78634, AoA_effective = -18345.02° could not be interpolated
Span position 134.36 mm, Re = 73126, AoA_effective = -18519.13° could not be interpolated
Span position 177.75 mm, Re = 67166, AoA_effective = -13185.02° could not be interpolated
Calculating Fin
Interpolating viscous properties …
Computing Plane for alpha=8.50° beta=0.00°
Calculating aerodynamic coefficients…
Calculating Main Wing
Interpolating viscous properties …
Span position -635.97 mm, Re = 83714, AoA_effective = 15.10° could not be interpolated
Span position -571.93 mm, Re = 88249, AoA_effective = 16.42° could not be interpolated
Span position -509.44 mm, Re = 92673, AoA_effective = 17.24° could not be interpolated
Span position -448.94 mm, Re = 96957, AoA_effective = 17.72° could not be interpolated
Span position -390.84 mm, Re = 101072, AoA_effective = 17.90° could not be interpolated
Span position -335.54 mm, Re = 104988, AoA_effective = 17.73° could not be interpolated
Span position -283.40 mm, Re = 108679, AoA_effective = 17.01° could not be interpolated
Span position -234.80 mm, Re = 112121, AoA_effective = 19.47° could not be interpolated
Span position -190.05 mm, Re = 115290, AoA_effective = 6510.17° could not be interpolated
Span position -149.48 mm, Re = 118163, AoA_effective = 13178.46° could not be interpolated
Span position -113.34 mm, Re = 120722, AoA_effective = 14676.54° could not be interpolated
Span position -81.90 mm, Re = 122948, AoA_effective = 14559.00° could not be interpolated
Span position -55.36 mm, Re = 124827, AoA_effective = 13989.52° could not be interpolated
Span position -33.91 mm, Re = 126346, AoA_effective = 13308.59° could not be interpolated
Span position -17.70 mm, Re = 127494, AoA_effective = 12734.06° could not be interpolated
Span position -6.82 mm, Re = 128264, AoA_effective = 12366.15° could not be interpolated
Span position -1.37 mm, Re = 128651, AoA_effective = 12212.55° could not be interpolated
Span position 1.37 mm, Re = 128651, AoA_effective = 12212.81° could not be interpolated
Span position 6.82 mm, Re = 128264, AoA_effective = 12366.72° could not be interpolated
Span position 17.70 mm, Re = 127494, AoA_effective = 12735.15° could not be interpolated
Span position 33.91 mm, Re = 126346, AoA_effective = 13309.78° could not be interpolated
Span position 55.36 mm, Re = 124827, AoA_effective = 13990.49° could not be interpolated
Span position 81.90 mm, Re = 122948, AoA_effective = 14559.25° could not be interpolated
Span position 113.34 mm, Re = 120722, AoA_effective = 14676.29° could not be interpolated
Span position 149.48 mm, Re = 118163, AoA_effective = 13175.22° could not be interpolated
Span position 190.05 mm, Re = 115290, AoA_effective = 6504.82° could not be interpolated
Span position 234.80 mm, Re = 112121, AoA_effective = 19.46° could not be interpolated
Span position 283.40 mm, Re = 108679, AoA_effective = 17.01° could not be interpolated
Span position 335.54 mm, Re = 104988, AoA_effective = 17.72° could not be interpolated
Span position 390.84 mm, Re = 101072, AoA_effective = 17.90° could not be interpolated
Span position 448.94 mm, Re = 96957, AoA_effective = 17.72° could not be interpolated
Span position 509.44 mm, Re = 92673, AoA_effective = 17.24° could not be interpolated
Span position 571.93 mm, Re = 88249, AoA_effective = 16.42° could not be interpolated
Span position 635.97 mm, Re = 83714, AoA_effective = 15.10° could not be interpolated
Calculating Elevator
Interpolating viscous properties …
Span position -177.75 mm, Re = 75536, AoA_effective = -14131.37° could not be interpolated
Span position -134.36 mm, Re = 82240, AoA_effective = -19849.65° could not be interpolated
Span position -94.26 mm, Re = 88435, AoA_effective = -19664.46° could not be interpolated
Span position -59.47 mm, Re = 93810, AoA_effective = -18117.49° could not be interpolated
Span position -31.72 mm, Re = 98097, AoA_effective = -16452.57° could not be interpolated
Span position -12.41 mm, Re = 101081, AoA_effective = -15224.72° could not be interpolated
Span position -2.51 mm, Re = 102611, AoA_effective = -14596.34° could not be interpolated
Span position 2.51 mm, Re = 102611, AoA_effective = -14596.84° could not be interpolated
Span position 12.41 mm, Re = 101081, AoA_effective = -15227.34° could not be interpolated
Span position 31.72 mm, Re = 98097, AoA_effective = -16455.24° could not be interpolated
Span position 59.47 mm, Re = 93810, AoA_effective = -18119.41° could not be interpolated
Span position 94.26 mm, Re = 88435, AoA_effective = -19665.65° could not be interpolated
Span position 134.36 mm, Re = 82240, AoA_effective = -19850.53° could not be interpolated
Span position 177.75 mm, Re = 75536, AoA_effective = -14131.79° could not be interpolated
Calculating Fin
Interpolating viscous properties …
Computing Plane for alpha=9.00° beta=0.00°
Calculating aerodynamic coefficients…
Calculating Main Wing
Interpolating viscous properties …
Span position -635.97 mm, Re = 100033, AoA_effective = 15.28° could not be interpolated
Span position -571.93 mm, Re = 105452, AoA_effective = 16.69° could not be interpolated
Span position -509.44 mm, Re = 110739, AoA_effective = 17.56° could not be interpolated
Span position -448.94 mm, Re = 115858, AoA_effective = 18.10° could not be interpolated
Span position -390.84 mm, Re = 120774, AoA_effective = 18.32° could not be interpolated
Span position -335.54 mm, Re = 125454, AoA_effective = 18.20° could not be interpolated
Span position -283.40 mm, Re = 129865, AoA_effective = 17.50° could not be interpolated
Span position -234.80 mm, Re = 133978, AoA_effective = 20.16° could not be interpolated
Span position -190.05 mm, Re = 137764, AoA_effective = 6952.58° could not be interpolated
Span position -149.48 mm, Re = 141197, AoA_effective = 14074.40° could not be interpolated
Span position -113.34 mm, Re = 144254, AoA_effective = 15674.23° could not be interpolated
Span position -81.90 mm, Re = 146915, AoA_effective = 15548.55° could not be interpolated
Span position -55.36 mm, Re = 149160, AoA_effective = 14940.25° could not be interpolated
Span position -33.91 mm, Re = 150975, AoA_effective = 14212.96° could not be interpolated
Span position -17.70 mm, Re = 152348, AoA_effective = 13599.34° could not be interpolated
Span position -6.82 mm, Re = 153268, AoA_effective = 13206.40° could not be interpolated
Span position -1.37 mm, Re = 153729, AoA_effective = 13042.35° could not be interpolated
Span position 1.37 mm, Re = 153729, AoA_effective = 13042.63° could not be interpolated
Span position 6.82 mm, Re = 153268, AoA_effective = 13207.00° could not be interpolated
Span position 17.70 mm, Re = 152348, AoA_effective = 13600.50° could not be interpolated
Span position 33.91 mm, Re = 150975, AoA_effective = 14214.23° could not be interpolated
Span position 55.36 mm, Re = 149160, AoA_effective = 14941.29° could not be interpolated
Span position 81.90 mm, Re = 146915, AoA_effective = 15548.82° could not be interpolated
Span position 113.34 mm, Re = 144254, AoA_effective = 15673.96° could not be interpolated
Span position 149.48 mm, Re = 141197, AoA_effective = 14070.95° could not be interpolated
Span position 190.05 mm, Re = 137764, AoA_effective = 6946.86° could not be interpolated
Span position 234.80 mm, Re = 133978, AoA_effective = 20.15° could not be interpolated
Span position 283.40 mm, Re = 129865, AoA_effective = 17.50° could not be interpolated
Span position 335.54 mm, Re = 125454, AoA_effective = 18.20° could not be interpolated
Span position 390.84 mm, Re = 120774, AoA_effective = 18.32° could not be interpolated
Span position 448.94 mm, Re = 115858, AoA_effective = 18.10° could not be interpolated
Span position 509.44 mm, Re = 110739, AoA_effective = 17.56° could not be interpolated
Span position 571.93 mm, Re = 105452, AoA_effective = 16.69° could not be interpolated
Span position 635.97 mm, Re = 100033, AoA_effective = 15.28° could not be interpolated
Calculating Elevator
Interpolating viscous properties …
Span position -177.75 mm, Re = 90261, AoA_effective = -15108.70° could not be interpolated
Span position -134.36 mm, Re = 98271, AoA_effective = -21224.06° could not be interpolated
Span position -94.26 mm, Re = 105674, AoA_effective = -21027.80° could not be interpolated
Span position -59.47 mm, Re = 112097, AoA_effective = -19375.09° could not be interpolated
Span position -31.72 mm, Re = 117220, AoA_effective = -17595.81° could not be interpolated
Span position -12.41 mm, Re = 120785, AoA_effective = -16283.53° could not be interpolated
Span position -2.51 mm, Re = 122613, AoA_effective = -15611.95° could not be interpolated
Span position 2.51 mm, Re = 122613, AoA_effective = -15612.48° could not be interpolated
Span position 12.41 mm, Re = 120785, AoA_effective = -16286.32° could not be interpolated
Span position 31.72 mm, Re = 117220, AoA_effective = -17598.66° could not be interpolated
Span position 59.47 mm, Re = 112097, AoA_effective = -19377.16° could not be interpolated
Span position 94.26 mm, Re = 105674, AoA_effective = -21029.07° could not be interpolated
Span position 134.36 mm, Re = 98271, AoA_effective = -21225.01° could not be interpolated
Span position 177.75 mm, Re = 90261, AoA_effective = -15109.15° could not be interpolated
Calculating Fin
Interpolating viscous properties …
Computing Plane for alpha=9.50° beta=0.00°
Calculating aerodynamic coefficients…
Calculating Main Wing
Interpolating viscous properties …
Span position -635.97 mm, Re = 138634, AoA_effective = 15.63° could not be interpolated
Span position -571.93 mm, Re = 146144, AoA_effective = 17.16° could not be interpolated
Span position -509.44 mm, Re = 153471, AoA_effective = 18.13° could not be interpolated
Span position -448.94 mm, Re = 160566, AoA_effective = 18.72° could not be interpolated
Span position -390.84 mm, Re = 167379, AoA_effective = 18.97° could not be interpolated
Span position -335.54 mm, Re = 173864, AoA_effective = 18.81° could not be interpolated
Span position -283.40 mm, Re = 179978, AoA_effective = 18.05° could not be interpolated
Span position -234.80 mm, Re = 185678, AoA_effective = 20.88° could not be interpolated
Span position -190.05 mm, Re = 190925, AoA_effective = 7408.45° could not be interpolated
Span position -149.48 mm, Re = 195683, AoA_effective = 14997.60° could not be interpolated
Span position -113.34 mm, Re = 199920, AoA_effective = 16702.27° could not be interpolated
Span position -81.90 mm, Re = 203607, AoA_effective = 16568.21° could not be interpolated
Span position -55.36 mm, Re = 206719, AoA_effective = 15919.92° could not be interpolated
Span position -33.91 mm, Re = 209235, AoA_effective = 15144.86° could not be interpolated
Span position -17.70 mm, Re = 211136, AoA_effective = 14490.96° could not be interpolated
Span position -6.82 mm, Re = 212412, AoA_effective = 14072.23° could not be interpolated
Span position -1.37 mm, Re = 213051, AoA_effective = 13897.42° could not be interpolated
Span position 1.37 mm, Re = 213051, AoA_effective = 13897.71° could not be interpolated
Span position 6.82 mm, Re = 212412, AoA_effective = 14072.88° could not be interpolated
Span position 17.70 mm, Re = 211136, AoA_effective = 14492.20° could not be interpolated
Span position 33.91 mm, Re = 209235, AoA_effective = 15146.22° could not be interpolated
Span position 55.36 mm, Re = 206719, AoA_effective = 15921.02° could not be interpolated
Span position 81.90 mm, Re = 203607, AoA_effective = 16568.50° could not be interpolated
Span position 113.34 mm, Re = 199920, AoA_effective = 16701.98° could not be interpolated
Span position 149.48 mm, Re = 195683, AoA_effective = 14993.92° could not be interpolated
Span position 190.05 mm, Re = 190925, AoA_effective = 7402.37° could not be interpolated
Span position 234.80 mm, Re = 185678, AoA_effective = 20.88° could not be interpolated
Span position 283.40 mm, Re = 179978, AoA_effective = 18.05° could not be interpolated
Span position 335.54 mm, Re = 173864, AoA_effective = 18.81° could not be interpolated
Span position 390.84 mm, Re = 167379, AoA_effective = 18.97° could not be interpolated
Span position 448.94 mm, Re = 160566, AoA_effective = 18.72° could not be interpolated
Span position 509.44 mm, Re = 153471, AoA_effective = 18.13° could not be interpolated
Span position 571.93 mm, Re = 146144, AoA_effective = 17.15° could not be interpolated
Span position 635.97 mm, Re = 138634, AoA_effective = 15.63° could not be interpolated
Calculating Elevator
Interpolating viscous properties …
Span position -177.75 mm, Re = 125092, AoA_effective = -16116.33° could not be interpolated
Span position -134.36 mm, Re = 136193, AoA_effective = -22641.13° could not be interpolated
Span position -94.26 mm, Re = 146452, AoA_effective = -22433.62° could not be interpolated
Span position -59.47 mm, Re = 155354, AoA_effective = -20671.91° could not be interpolated
Span position -31.72 mm, Re = 162454, AoA_effective = -18774.66° could not be interpolated
Span position -12.41 mm, Re = 167394, AoA_effective = -17375.34° could not be interpolated
Span position -2.51 mm, Re = 169928, AoA_effective = -16659.24° could not be interpolated
Span position 2.51 mm, Re = 169928, AoA_effective = -16659.81° could not be interpolated
Span position 12.41 mm, Re = 167394, AoA_effective = -17378.33° could not be interpolated
Span position 31.72 mm, Re = 162454, AoA_effective = -18777.70° could not be interpolated
Span position 59.47 mm, Re = 155354, AoA_effective = -20674.11° could not be interpolated
Span position 94.26 mm, Re = 146452, AoA_effective = -22434.98° could not be interpolated
Span position 134.36 mm, Re = 136193, AoA_effective = -22642.14° could not be interpolated
Span position 177.75 mm, Re = 125092, AoA_effective = -16116.81° could not be interpolated
Calculating Fin
Interpolating viscous properties …
Computing Plane for alpha=10.00° beta=0.00°
Panel Analysis completed … Errors encountered
Cleaning up
Analysis ended 13 June 2020 23:08:39
Elapsed: 7.36 s

André Deperroistechwinder Staff replied 1 month ago

Hello,
Difficult to say what the problem is without seeing the model. The things to do
– run the analysis in inviscid mode, generate the operating point and check that the gamma colour map is smooth; local colour peaks may indicate where the problem is
– check that the fuselage is well connected to the wings, using the “connect” and “check free edges” menu items.
– instead of interpolating using the strip’s apparent aoa, select interpolate “from Cl – xflr5 method” in the analysis definition form
– if you can’t work it out, please share the project file; you can send it to the contact address for technical questions; all models are kept strictly confidential
André