The current scope, recent progress, and plans for research and development of computational methods for unsteady aerodynamics at the NASA Langley Research Center are reviewed. Both integral-equations and finite-difference method for inviscid and viscous flows are discussed. Although the great bulk of the effort has focused on finite-difference solution of the transonic small-perturbation equation, the integral-equation program is given primary emphasis here because it is less well known.


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    Title :

    Development of Computational Methods for Unsteady Aerodynamics at the NASA (National Aeronautics and Space Administration) Langley Research Center


    Contributors:
    E. C. Yates (author) / W. Whitlow (author)

    Publication date :

    1987


    Size :

    22 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English