EXPERIMENTAL AND THEORETICAL INVESTIGATIONS TO DEVELOP A MODEL OF ROTOR AERODYNAMICS ADAPTED TO STEEP DESCENTS
Annual forum; 58th, American Helicopter Society ; 2002 ; Montreal, Canada
2002-01-01
14 pages
Also known as FORUM 58
Conference paper
English
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DEPARTMENTS - Rotary Wing Aircraft in Steep Descents
Online Contents | 2001
Theoretical and Experimental Studies on Unsteady Rotor-Fuselage Interactional Aerodynamics
British Library Conference Proceedings
|THE INVESTIGATION OF ROTOR’S INFLOW AND MAIN ROTOR’S INDUCED VELOCITY AT HOVER AND AT STEEP DESCENTS
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|Experimental aerodynamics of a rotor entry vehicle
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