The flow field about a delta wing equipped with thrust reverser jets in slow speed flight near the ground has been computed. Results include the prediction of the flow about the delta wing at four fixed heights above the ground, and a simulated landing, in which the delta wing descends towards the ground. Comparison of computed and experimental lift coefficients indicates that the simulations can capture at least the qualitative trends in lift-loss encountered by thrust-vectoring aircraft operating in ground effect.


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    Titel :

    Numerical simulation of STOL operations using thrust-vectoring


    Beteiligte:

    Kongress:

    AIAA, Aircraft Design Systems Meeting ; 1992 ; Hilton Head Island, SC, United States


    Erscheinungsdatum :

    01.08.1992


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Numerical simulation of STOL operations using thrust-vectoring

    CHAWLA, KALPANA / VAN DALSEM, W. | AIAA | 1992


    Application of thrust vectoring for STOL

    Whitten, P. D. / Woodrey, R. W. / Hames, J. E. | NTRS | 1981


    Application of thrust vectoring for STOL

    WHITTEN, P. / WOODREY, R. / HAMES, J. | AIAA | 1981


    Development of Thrust Deflection and Vectoring - V/STOL

    Smith, A. D. F. | SAE Technical Papers | 1966


    STOL Transport Thrust Reverser/Vectoring Program. Volume II

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