Using Mesh Adjoint for Shock Bump Deployment and Optimisation on Transonic Wings (AIAA 2015-1488)
Aerospace sciences meeting
01.01.2015
18 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Transonic Flutter Characteristics of Advanced Fighter Wings (AIAA 2015-0438)
British Library Conference Proceedings | 2015
|Effect of Vortex Generators on Transonic Swept Wings (AIAA 2015-1238)
British Library Conference Proceedings | 2015
|Analysis of the Transonic Flutter of Supersonic Transport Wings (AIAA 2015-0443)
British Library Conference Proceedings | 2015
|Aeroelastic Tailoring of Transport Wings Including Transonic Flutter Constraints (AIAA 2015-1127)
British Library Conference Proceedings | 2015
|