The mixed elliptic-hyperbolic relaxation method for obtaining steady-state solutions to two-dimensional transonic potential equations is extended to the transonic small disturbance equation in three dimensions. In particular, transonic flow is considered both about nonlifting wing-cylinder combinations and over thin lifting wings with sweep and taper. The treatment is restricted to freestream Mach numbers less than one and to wings with subsonic trailing edges.


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    Title :

    Relaxation methods for transonic flow about wing-cylinder combinations and lifting swept wings


    Contributors:

    Conference:

    International Conference on Numerical Methods in Fluid Mechanics ; 1972 ; Paris, France


    Publication date :

    1973-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :