Aerodynamic force and inlet pressure data are obtained for 9.5% force and pressure models of a V/STOL fighter/attack aircraft configuration with top mounted twin inlets. Data are presented from tests conducted in the Ames Unitary Wind Tunnels at Mach numbers of 0.6, 0.9, and 1.2 at angles of attack up to 27 deg. and angles of sideslip up to 12 deg. Trimmed aerodynamic characteristics and inlet performance are compared for three different leading edge extension (LEX) configurations. The effects of wing leading and trailing-edge flaps on the inlet are also determined. Maneuver perfromance is calculated form combined force and inlet pressure data. The largest of the three LEX sizes tested gives the best airplane maneuver performance. Wing flap deflections improved inlet recovery at all Mach numbers.


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    Titel :

    Inlet and airframe compatibility for a V/STOL fighter/attack aircraft with top-mounted inlets


    Beteiligte:
    Durston, D. A. (Autor:in) / Smeltzer, D. B. (Autor:in)

    Erscheinungsdatum :

    1982-06-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :




    Airframe effects on top-mounted inlet systems for VSTOL fighter aircraft

    SMELTZER, D. / NELMS, W. / WILLIAMS, T. | AIAA | 1981


    Airframe effects on top-mounted inlet systems for VSTOL fighter aircraft

    Smeltzer, D. B. / Nelms, W. P. / Williams, T. L. | NTRS | 1981


    Airframe effects on a top-mounted fighter inlet system

    Smeltzer, D. B. / Nelms, W. P. / Williams, T. L. | NTRS | 1982