Wing design by solving adjoint equations
40th AIAA Aerospace Sciences Meeting & Exhibit ; 2002 ; Reno , NV , U.S.A.
01.01.2002
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Design of Adjoint Based Laws for Wing Flutter Control
AIAA | 2009
|Design of Adjoint-Based Laws for Wing Flutter Control
AIAA | 2011
|Design of Adjoint Based Laws for Wing Flutter Control
British Library Conference Proceedings | 2009
|Aerostructural Adjoint Method for Flexible Wing Optimization
British Library Conference Proceedings | 2012
|