Details are given of the expressions used to describe the aerodynamics and kinematics of the Sea King Mk.50 helicopter during steady flight and low rate maneuvers up to an advance ratio of 0.3. The aerodynamics/kinematics formulation is a major component of the Sea King mathematical model developed by Aeronautical Research Laboratories (ARL) for flight simulation of this anti-submarine warfare helicopter.
Mathematical Model of the Sea King MK.50 Helicopter Aerodynamics and Kinematics
1986
63 pages
Report
No indication
English
Unsteady Aerodynamics of Helicopter Rotors: Mathematical Models
British Library Conference Proceedings | 1995
|NTIS | 1972
|TIBKAT | 1972
|NTIS | 1971
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