NLF Airfoil and Wing Design by Adjoint Method and Automatic Transition Prediction
27th AIAA Applied Aerodynamics Conference
2009-01-01
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
|