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Verified Commit 3b935a0e authored by Paul Dechamps's avatar Paul Dechamps :speech_balloon:
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(feat) Added MDAO api for aerodynamics optimization 

The api features 3 components: The solver, the geometry and the initial mesh. The api is tested in a aerodynamic shape case where the NACA0012 is constrained at 0deg AoA with cl=0.40 and the objective function to minimize is the drag wrt the max camber and the max camber position. The test case ends with a final shape close to the NACA4412 (camber = 35% & max camber pos = 41%)
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1 merge request!1BLASTER v1.0
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