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    Wind-shear endurance capability for powered-lift aircraft

    Wind-shear endurance capability for powered-lift aircraft


    The present treatment of safety margin considerations for powered-lift (upper wing surface blowing) STOL aircraft emphasizes wind shear endurance, in order to establish safety margin criteria for such aircraft that are equivalent to those of conventional transport aircraft. The simulation results obtained show that a 6.6 deg climb gradient at V(app) for STOL aircraft is required for equivalent shear endurance in approaching a long STOL airport runway, if the STOL aircraft is equipped with an elaborate control/display system and is permitted a change in configuration.

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    Titel :

    Wind-shear endurance capability for powered-lift aircraft

    Beteiligte:
    Bando, Toshio (Autor:in) / Tanaka, Keiji (Autor:in) / Hynes, Charles S. (Autor:in) / Hardy, Gordon H. (Autor:in)
    Erschienen in:

    In: AIAA Atmospheric Flight Mechanics Conference, Monterey, CA, Aug. 9-11, 1993, Technical Papers (A93-48301 20-08)

    Erscheinungsdatum :

    1993-01-01

    Medientyp :

    Aufsatz (Konferenz)

    Format :

    Keine Angabe

    Sprache :

    Englisch

    Schlagwörter :

    Aircraft Stability And Control

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