Automated Trailing-Edge Flap for Airfoil Drag Reduction over a Large Lift-Coefficient Range
20th AIAA Applied Aerodynamics Conference ; 2002 ; St. Louis , Missouri
2002-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
FULL-LENGTH PAPERS - Automated Cruise Flap for Airfoil Drag Reduction over a Large Lift Range
Online Contents | 2002
|Effect of multiple fixed slots and trailing-edge flap on lift and drag of Clark Y airfoil
Engineering Index Backfile | 1932
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