Results of NASA Langley has conducted wind-tunnel investigations of several fighter configurations conducted to determine the effects of both thrust vectoring and spanwise blowing are reviewed. A recent joint NASA/Grumman Aerospace Corporation/U.S. Air Force Wright Aeronautical Laboratory wind-tunnel investigation was conducted to examine the effects of spanwise blowing on the trailing-edge flap system. This application contrasts with the more familiar method of spanwise blowing near the wing leading edge. Another joint program among NASA/McDonnell Aircraft Company/U.S. Air Force Wright Aeronautical Laboratory investigated the effects of reverse thrust on the low-speed aerodynamics of an F-15 configuration. The F-15 model was fitted with a rotating van thrust reverser concept which could simulate both in-flight reversing for approach and landing or full reversing for ground roll reduction. The significant results of these two joint programs are reported.


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    Titel :

    Thrust-Induced Effects on Low-Speed Aerodynamics of Fighter Aircraft


    Beteiligte:
    D. W. Banks (Autor:in) / P. F. Quinto (Autor:in) / J. W. Paulson (Autor:in)

    Erscheinungsdatum :

    1982


    Format / Umfang :

    25 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Thrust-induced effects on low-speed aerodynamics of fighter aircraft

    Banks, D. W. / Quinto, P. F. / Paulson, J. W., Jr. | NTRS | 1981


    Thrust-induced effects on low-speed aerodynamics of fighter aircraft

    BANKS, D. / QUINTO, P. / PAULSON, JR., J. | AIAA | 1981


    Thrust-induced effects on low-speed aerodynamics of fighter aircraft

    Banks, D. W. / Quinto, P. F. / Paulson, J. W., Jr. | NTRS | 1982


    Thrust reverser effects on fighter aircraft aerodynamics

    GLEZER, A. / HUGHES, R. V. / HUNT, B. L. | AIAA | 1985


    Effects of spanwise blowing and reverse thrust on fighter low-speed aerodynamics

    PAULSON, J. W. / BANKS, D. W. / QUINTO, P. F. | AIAA | 1983