OpenAeroStruct
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Add stability-constrained examples
Description of feature
Add examples and documentation of analysis/optimization with stability derivatives. It requires nesting OM problems. Reference: https://github.com/OpenMDAO/RevHack2020/tree/master/problems/oas_stability_derivs
Also, the origin for the chordwise coordinate should be documented. I believe the default origin is at LE for rectangular wing and nose for CRM, but I should double check.