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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    Titel :

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


    Beteiligte:

    Erscheinungsdatum :

    1989


    Format / Umfang :

    25 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Oscillating wings in compressible subsonic flow

    Jones, W. P. / Aeronautical Research Council | TIBKAT | 1957


    Oscillating wings and bodies with flexure in supersonic flow

    LIU, D. D. / GARCIA-FOGEDA, P. / CHEN,P. C. | AIAA | 1988


    Oscillating wings in compressible subsonic flow

    Jones, William Neville Prichard | SLUB | 1957