NLF Airfoil and Wing Design by Adjoint Method and Automatic Transition Prediction
27th, AIAA Applied Aerodynamics Conference ; 2009 ; San Antonio, TX
2009-01-01
27 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Natural-Laminar-Flow Airfoil and Wing Design by Adjoint Method and Automatic Transition Prediction
British Library Conference Proceedings | 2009
|