Analysis tools and modeling concepts for jet flow fields encountered upon use of thrust reversers for high performance military aircraft are described. A semi-empirical model of the reverser ground wall jet interaction with the uniform cross flow due to aircraft forward velocity is described. This ground interaction model is used to demonstrate exhaust gas ingestion conditions. The effects of control of exhaust jet vector angle, lateral splay, and moving versus fixed ground simulation are discussed. The Adler/Baron jet-in-cross flow model is used in conjunction with three dimensional panel methods to investigate the upper surface jet induced flow field.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    STOL landing thrust: Reverser jet flowfields


    Beteiligte:
    Kotansky, D. R. (Autor:in) / Glaze, L. W. (Autor:in)


    Erscheinungsdatum :

    01.02.1987


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    STOL Landing Thrust: Reverser Jet Flowfields

    D. R. Kotansky / L. W. Glaze | NTIS | 1987


    STOL Transport Thrust Reverser/Vectoring Program. Volume II

    J. E. Petit / M. B. Scholey | NTIS | 1973


    A method for increasing thrust reverser utilization on STOL aircraft

    TATOM, J. / DUNLAP, J. / LEDWITH, W. | AIAA | 1972


    A method for increasing thrust reverser utilization on STOL aircraft.

    Tatom, J. W. / Dunlap, J. H. / Ledwith, W. A. | NTRS | 1972