The paper takes a brief look at powered lift from the point of view of the operator and the designer, considers application of an ejector-powered lift system to both STOL and VTOL aircraft, and describes some of the advantages of an ejector concept. Performance and noise characteristics of a simple ejector are described, and some comments are made regarding the Buffalo/Spey Augmentor-Wing proof-of-concept aircraft.


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    Titel :

    Ejector-powered lift systems for V/STOL aircraft


    Beteiligte:

    Erscheinungsdatum :

    01.05.1974


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Powered lift aerodynamics of USB STOL aircraft

    MAITA, M. / FUJIEDA, H. / MORITA, M. et al. | AIAA | 1983


    Safety considerations for powered-lift STOL aircraft

    Holzhauser, C. A. / Innis, R. C. | NTRS | 1971



    Operational experience with a powered-lift STOL aircraft

    Innis, R. C. / Quigley, H. C. | NTRS | 1976