共 16 条
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Separation control using plasma actuators: dynamic stall vortex control on oscillating airfoil. ML Post,TC Corke. AIAA Journal . 2006
[2]
The Helicopter. Leishman J G. . 2007
[3]
A review of compressible dynamic stall control principles and methods. Chandrasekhara M. Proceedings of the Tenth Asian Congress of Fluid Mechanics . 2004
[4]
A 2-d dynamic stall model based on a hopf bifurcation. Truong V K. ONERA-TAP--93-156 . 1994
[5]
NACA64A006,Oscillating flap. Zwaan R J. AGARD R-702 . 1982
[6]
A qualitative examination of dynamic stall from flight test data. Bousman W G. J AHS . 1998
[7]
"The Effect of a Leading Edge Slat on Dynamic Stall of an oscillating Airfoil". Carr,L.W,McAlister,K.W. AIAA Paper83-2533 . 1983
[8]
"Dynamic Stall Control Investigations on a Full Size Chord Blade Section". Geissler,W,Dietz,G,Mai,H,Junker,B,Lorkows-ki,T. 30th European Rotorcraft Fo-rum . 2004
[9]
Parametric Study of an Air-Jet Vortex Generator Configuration to Control Rotorcraft Retreating Blade Stall. Chrisminder Singh,David J. Peake. AIAA 2005-1366 .
[10]
A parametric design study for a swashplateless helicopter rotor with trailing-edge flaps. Shen J W,Chopra I. Journal of the American Helicopter Society . 2004