TAWFIVE computer program calculates transonic flow over transport-type wing and fuselage. Combines multigrid acceleration technique in iterative solution of potential equation with use of integral-form boundary-layer equations to provide software tool computationally efficient, yet accurate enough for use in design. Simplifies solution process by breaking problem into loosely coupled set of modified equations. Inviscid-flow method, using standard inviscid-flow equations, valid in "outer" region away from wing, whereas boundary-layer equations valid in thin region near solid surface of wing. Written in FORTRAN 77.


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    Title :

    Analyzing Transonic Flow Over A Wing And Fuselage


    Contributors:

    Published in:

    Publication date :

    1993-02-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :




    Transonic Navier-Stokes flow computations over wing-fuselage geometries

    Agrawal, S. / Vatsa, V. N. / Kinard, T. A. | NTRS | 1993


    Transonic Navier-Stokes Flow Computations over Wing-Fuselage Geometries

    Agrawal, S. / Kinard, T. / Vatsa, V. et al. | British Library Conference Proceedings | 1991


    Transonic Navier-Stokes flow computations over wing-fuselage geometries

    AGRAWAL, S. / VATSA, V. N. / KINARD, T. A. | AIAA | 1972