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@mvanzulli mvanzulli commented Sep 7, 2022

This PR close a subtask of #363. A validation example will be added further on. Note that I've added a new field in elemTypeAero field

computeAeroTangMatrix = false ;
elements(2).elemTypeAero   = [0 dext 0 numGaussPoints computeAeroTangMatrix];

According to my non-extensive tests the computation of the tangent matrix can induce a significant performance penalty. But now the nonLinearAerodynamics static example resits until 100m/s 💯

Thanks to @jorgepz and @TheChikenfly for the discussion.

@mvanzulli mvanzulli marked this pull request as ready for review September 8, 2022 01:35
@mvanzulli mvanzulli merged commit 946ba8f into master Sep 8, 2022
@jorgepz jorgepz deleted the addTangentAero branch September 8, 2022 13:55
@TheChikenfly
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nice work!

@jorgepz
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jorgepz commented Sep 8, 2022

Thanks!

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4 participants