Aerostructural analysis (both tubular and wingbox) does not work with right-side symmetric wings. Currently, only the aerodynamic analysis/optimization can handle right-side wings as fixed in PR #381 .
Most of the examples in OAS use left-side symmetric wing, therefore this bug does not affect most of the cases.
Exception is the OpenVSP-generated symmetric wings, which sit on the right-side plane (as reported in #396 )
Steps to reproduce issue
Copy any aerostructural example with a symmetric wing, and flip the mesh to obtain the right-side mesh:
mesh = mesh[:, ::-1, :]
mesh[:, :, 1] *= -1.0
Run aerostructural analysis with the flipped mesh.
Current behavior
Aerostructural solver fails.
Expected behavior
The right-side wing results should be the same as the original left-wing results.
Description
Aerostructural analysis (both tubular and wingbox) does not work with right-side symmetric wings. Currently, only the aerodynamic analysis/optimization can handle right-side wings as fixed in PR #381 .
Most of the examples in OAS use left-side symmetric wing, therefore this bug does not affect most of the cases. Exception is the OpenVSP-generated symmetric wings, which sit on the right-side plane (as reported in #396 )
Steps to reproduce issue
Current behavior
Aerostructural solver fails.
Expected behavior
The right-side wing results should be the same as the original left-wing results.
Code versions