Aerostructural Adjoint Method for Flexible Wing Optimization-Reference-Cited by-同舟云学术

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Aerostructural Adjoint Method for Flexible Wing Optimization

Published:2012-04-23 Issue: Volume: Page:
ISSN:
Container-title:53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference<BR>20th AIAA/ASME/AHS Adaptive Structures Conference<BR>14th AIAA
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Author:

Ghazlane Imane,Carrier Gerald,Dumont Antoine,Desideri Jean-antoine

Publisher

American Institute of Aeronautics and Astronautics

Reference11 articles.

1. 1DumontA., GhazlaneI., MarceletM., CarrierG., SalahElDinI., OverviewofRecentDevelopmentofAeroelasticAdjointMethodforCivil AircraftWingOptimizationatOnera., ONERA-DLRAerospaceSymposium,ODAS2011

2. 15Marcelet M., Peter J., Carrier G., Sensitivity analysis of a coupled aero-structural system using direct differentiation and adjoint method, ECCOMASCFD2006.

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