RHOIV computer program predicts unsteady lifting-surface loadings caused by motions of leading edge and trailing-edge control surfaces having sealed gaps at hinge lines and side edges. Analysis is based on linear, subsonic, potential-flow theory using kernel function method. Linear combinations of pressure distributions are used that are continuous except at planform edges and hinge lines. Loading solution is obtained by downwash collocation for deflection or motion of main wing and control surfaces.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Unsteady Subsonic Loadings Due to Control-Surface Motion


    Contributors:
    Rowe, W. S. (author)

    Published in:

    Publication date :

    1982-09-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :