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Title: tese_paulo_asaquebra Download
 Description: MATLAB code for optimal design of transonic wings. Optimize the wing parameters considering the better specific range. Master dissertation of Paulo Ferrucio
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trabalhoFIM444.m
trabalhoFIM.m
trabalhoFIMpolar.m
trabalhoFIMsubida.m
trabalhoFIMteste.m
trabalhoFIM1.m
trabalhoFIM11.m
trabalhoFIM44.m
mattos_AIAA-2004-5191-321.pdf

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