Unsteady aerodynamic and stall effects on helicopter rotor blade airfoil sections.
LIIVA, J. /BOEING CO., VERTOL DIV., AERODYNAMIC RESEARCH UNIT, PHILADELPHIA, PA./.
Journal of Aircraft ; 6 , 1 ; 46-51
1969
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
GenHel Rotor Blade Airfoil Unsteady Aerodynamic Model
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