Aircraft geometry requirements for unsteady aerodynamic computations are discussed and differences between requirements for steady and unsteady flow are emphasized within the framework of a general potential-flow aerodynamic formulation. Its implementation in a computer program called SOUSSA (Steady, Oscillatory, and Unsteady Subsonic and Supersonic Aerodynamic is detailed.


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    Title :

    Geometry requirements for unsteady aerodynamics in aeroelastic analysis and design


    Contributors:

    Publication date :

    1978-09-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :