Questions, suggestions, feature requests, bug reports, feedback Filter:AllOpenResolvedClosedUnansweredSort byViewsAnswersVotesDifference between Cd_i and Cd_vClosedHiroshi Takeuchi asked 2 years ago • Questions351 views0 answers0 votesLinear density triangular panel method is crashing when I'm trying to run it with thick wingsOpenAaditya Wangikar asked 2 years ago • Questions339 views0 answers0 votesImporting Plane Definition file overwrites airfoil polars.OpenJoão Hackbart asked 2 years ago • Questions364 views3 answers0 votesAny description / explanation of spanwise oppoints output numbers such as Vd.x and F.xClosedHiroshi Takeuchi asked 2 years ago • Questions337 views0 answers0 votesfuselage and wing analysis errorAnsweredAbhishek Rai asked 2 years ago • Questions348 views1 answers0 votes
Hiroshi Takeuchi