Questions, suggestions, feature requests, bug reports, feedback Filter:AllOpenResolvedClosedUnansweredSort byViewsAnswersVotesDifference between Cd_i and Cd_vClosedHiroshi Takeuchi asked 7 months ago • Questions131 views0 answers0 votesLinear density triangular panel method is crashing when I'm trying to run it with thick wingsOpenAaditya Wangikar asked 8 months ago • Questions127 views0 answers0 votesImporting Plane Definition file overwrites airfoil polars.OpenJoão Hackbart asked 8 months ago • Questions151 views3 answers0 votesAny description / explanation of spanwise oppoints output numbers such as Vd.x and F.xClosedHiroshi Takeuchi asked 9 months ago • Questions146 views0 answers0 votesfuselage and wing analysis errorAnsweredAbhishek Rai asked 9 months ago • Questions162 views1 answers0 votes
Hiroshi Takeuchi