Using Mesh Adjoint for Shock Bump Deployment and Optimisation on Transonic Wings
53rd AIAA Aerospace Sciences Meeting
01.01.2015
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Using Mesh Adjoint for Shock Bump Deployment and Optimisation on Transonic Wings (AIAA 2015-1488)
British Library Conference Proceedings | 2015
|``Bump'' As a Shock Control Device at Transonic Speeds
British Library Conference Proceedings | 2012
|An adaptive bump for transonic shock wave drag reduction
Tema Archiv | 2002
|