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Monitor outputs #30

Answered by EdoAlvarezR
juddmehr asked this question in Q&A
Aug 16, 2021 · 1 comments · 1 reply
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If I understand correctly, you are trying to obtain the effective velocity along the wing and decompose into arbitrary direction, right?

For debugging purposes, I exposed the effective velocities used in the force calculation in calc_aerodynamicforce(...) through the optional argument Vout. Notice in Line 81 that if Vout is different than nothing, it will push to it an array with the vectors of the VPM-induced velocity (wake and embedded particles), VLM-induced velocity, freestream, and local kinematic velocity, all evaluated at the mid-point of the three bound vortices that make each horseshoe (TE to 1/4 chord, lifting line at 1/4 chord, and 1/4 chord to TE).

Hence, unfolding the two for

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juddmehr Aug 18, 2021
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