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Update README.md
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gjkennedy authored Jun 26, 2024
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# "Super Simple" Wing
# Simple Subsonic Wing
Testing out fully-coupled aeroelastic optimizations on a simple wing geometry.

## Preliminary Sizing
Expand All @@ -18,4 +18,4 @@ Twist variable is not used at root station (fixed there)
Putting it all together
* 5_shape_and_struct.py - geom twist variables + panel thickness struct variables
* 6_shape_and_aero.py - geom twist variables + aero aoa variable + airfoil thickness
* 7_kitchen_sink.py - put all previous variables together : geom twist, airfoil thickness, AOA, panel thickness
* 7_kitchen_sink.py - put all previous variables together : geom twist, airfoil thickness, AOA, panel thickness

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