Investigation of rotor contribution to stability derivatives of aircraft at high rotor inflow ratio conditions made; analytical expressions for evaluating rotor stability derivatives developed for hovering, transitional, and high speed flight regimes; error in estimating rotor derivatives by application of small angle assumption is determined.
Rotor stability derivatives at high inflow ratio conditions for tilt rotor VTOL aircraft
Am Helicopter Soc -- J
American Helicopter Society -- Journal ; 7 , n 2
1962
12 pages
Article (Journal)
English
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