NLF Airfoil and Wing Design by Adjoint Method and Automatic Transition Prediction
27th AIAA Applied Aerodynamics Conference
01.01.2009
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
NLF Airfoil and Wing Design by Adjoint Method and Automatic Transition Prediction
British Library Conference Proceedings | 2009
|Natural-Laminar-Flow Airfoil and Wing Design by Adjoint Method and Automatic Transition Prediction
British Library Conference Proceedings | 2009
|