The development of VTOL technology over a thirty year period was reviewed. Various powered-lift concepts were explored and recent application analyzed. The ACSYNT computer program, developed by the NASA Ames Research Center, was used to predict the takeoff performance of a proposed jet STOL transport utilizing the Lockheed AIBF system. A correlation of the performance of the S-3A VIKING aircraft was performed. (DePo)


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    Titel :

    Application of powered high lift systems to STOL aircraft design


    Weitere Titelangaben:

    Anwendung des Hochleistungs-Auftriebsystems beim Entwurf von Kurzstartflugzeugen STOL


    Beteiligte:
    Ameel, F.D. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1979


    Format / Umfang :

    215 Seiten


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch





    Safety considerations for powered-lift STOL aircraft

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


    Powered lift aerodynamics of USB STOL aircraft

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


    Approach path control for powered-lift STOL aircraft

    Clymer, D. J. / Flora, C. C. | NTRS | 1973


    Approach Path Control for Powered-Lift STOL Aircraft

    D. J. Clymer / C. C. Flora | NTIS | 1973