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Aeroelastic coupling in sonic boom optimization of a supersonic aircraft

Abstract : In this paper, we consider a multi-disciplinary optimization problem where the initial shape of a wing is sought in order to cope, after elastic deformation by the flow, with some optimality conditions. We propose a medium-strong coupling which allows to consider different softwares communicating a small number of times. Applications to the optimization of the AGARD Wing 445.6 and a flexible supersonic aircraft wing are presented.
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https://hal.inria.fr/inria-00071718
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Submitted on : Tuesday, May 23, 2006 - 6:36:05 PM
Last modification on : Friday, February 4, 2022 - 3:15:58 AM
Long-term archiving on: : Sunday, April 4, 2010 - 10:34:52 PM

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  • HAL Id : inria-00071718, version 1

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Mariano Vázquez, Alain Dervieux, Bruno Koobus. Aeroelastic coupling in sonic boom optimization of a supersonic aircraft. [Research Report] RR-4865, INRIA. 2003. ⟨inria-00071718⟩

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