Basic conditions, study parameters, and various solutions of fighter intake and afterbody (except VTOL) are reviewed. Airframe integration and intake adaptation to the flight Mach number are discussed. The following topics of intake flow are analyzed: buzz phenomena, internal bleed flow, high incidence, low speed, mean flow, distortion index, and unsteady distortion. The afterbody discussion covers variable geometry, thrust vectoring, and reverse. Wind tunnel test techniques are also described.


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    Titel :

    Fundamentals of Fighter Aircraft Design: Engine Intake and Afterbody


    Beteiligte:
    J. Leynaert (Autor:in)

    Erscheinungsdatum :

    1987


    Format / Umfang :

    39 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






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