Skip to Main content Skip to Navigation
Reports

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.
Document type :
Reports
Complete list of metadata

Cited literature [1 references]  Display  Hide  Download

https://hal.inria.fr/inria-00071718
Contributor : Rapport de Recherche Inria <>
Submitted on : Tuesday, May 23, 2006 - 6:36:05 PM
Last modification on : Monday, July 23, 2018 - 2:20:01 PM
Long-term archiving on: : Sunday, April 4, 2010 - 10:34:52 PM

Identifiers

  • HAL Id : inria-00071718, version 1

Collections

Citation

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

Share

Metrics

Record views

205

Files downloads

255