Aerostructural optimization of the Common Research Model configuration


The NASA Common Research Model (CRM) has become a standard test case for verification and validation of Reynolds averaged Navier–Stokes computational fluid dynamics codes. In this paper we evaluate the suitability of the CRM for aerostructural and aeroelastic optimization studies. Since the CRM was originally intended for aerodynamic studies only, the… (More)


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@inproceedings{Kenway2014AerostructuralOO, title={Aerostructural optimization of the Common Research Model configuration}, author={Gaetan K.W. Kenway and Joaquim R. R. A. Martins and Graeme J. Kennedy}, year={2014} }