Unsteady aerodynamic loads in the subsonic and supersonic domain have been obtained with two new panel methods for lifting surfaces and for realistic aircraft configurations. A description of the methods is given. Results are presented and comparisons are made with results of existing methods and with experimental data for a fighter-type wing with external stores.


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    Title :

    Calculation of Unsteady Subsonic and Supersonic Flow about Oscillating Wings and Bodies by New Panel Methods


    Contributors:

    Publication date :

    1989


    Size :

    25 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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    Oscillating wings in compressible subsonic flow

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