Piloted simulator tests on the NASA-Ames Flight Simulator for Advanced Aircraft motion base played a major role in guiding the design of the Modified C-8A 'Buffalo' augmentor wing jet flap STOL research airplane. Design results are presented for the flight control systems, lateral-directional SAS, hydraulic systems, and engine and thrust vector controls. Emphasis is given to lateral control characteristics on STOL landing approach, engine-out control and recovery techniques in the powered-lift regime, and operational flight procedures which affected airplane design.


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    Titel :

    Use of the flight simulator in the design of a STOL research aircraft.


    Beteiligte:
    Spitzer, R. E. (Autor:in) / Rumsey, P. C. (Autor:in) / Quigley, H. C. (Autor:in)

    Kongress:

    American Institute of Aeronautics and Astronautics, Aircraft Design, Flight Test, and Operations Meeting ; 1972 ; Los Angeles, CA


    Erscheinungsdatum :

    01.08.1972


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Flight research using V/STOL simulator

    McGregor, D.M. | Engineering Index Backfile | 1965


    Use of the flight simulator in the design of a STOL research aircraft

    SPITZER, R. / RUMSEY, P. / QUIGLEY, H. | AIAA | 1972



    Flight directors for STOl aircraft

    Rabin, U. H. | NTRS | 1983


    Flight director design for a STOL aircraft.

    Seitz, W. R. / Goodson, R. E. | NTRS | 1973