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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Mathematical Model of the Sea King MK.50 Helicopter Aerodynamics and Kinematics


    Contributors:

    Publication date :

    1986


    Size :

    63 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





    Unsteady Aerodynamics of Helicopter Rotors: Mathematical Models

    Kritsky, B. / Loktev, B. / Nisht, M. et al. | British Library Conference Proceedings | 1995


    Helicopter Aerodynamics

    D. I. Bazov | NTIS | 1972


    Helicopter aerodynamics

    Bazov, D. I. | TIBKAT | 1972


    Helicopter Aerodynamics

    D. I. Bazov | NTIS | 1971