A numerical method to obtain a complete solution for the dynamic response of a variable sweep wing aircraft while changing the angle of sweep is presented. Both aerodynamic and trajectory computations are included. During the flight of the sweptback angle variation, the aerodynamic forces acting on the aircraft are obviously unsteady, therefore, methods for computing these forces and accompanying responses of aircraft are also presented.


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    Title :

    Influence of Unsteady Aerodynamic Forces on Dynamic Response of Variable Sweep Aircraft (Abstract Only)


    Contributors:
    M. Yan (author) / C. Qiu (author)

    Publication date :

    1987


    Size :

    1 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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