Adjoint-Based Optimisation of a Blended Wing Body Aircraft with Shock Control Bumps
45th AIAA Aerospace Sciences Meeting and Exhibit
01.01.2007
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Parallel adjoint-based optimisation of a blended wing body aircraft with shock control bumps
Online Contents | 2007
|Adjoint-Based Optimisation of a Blended Wing Body Aircraft with Shock Control Bumps AIAA Paper
British Library Conference Proceedings | 2007
|