A fixed-base simulator study was conducted to determine the flight characteristics of a representative STOL transport having a high wing and equipped with an external-flow jet flap in combination with four high-bypass-ratio fan-jet engines during the approach and landing. Real-time digital simulation techniques were used. The computer was programed with equations of motion for six degrees of freedom and the aerodynamic inputs were based on measured wind-tunnel data. A visual display of a STOL airport was provided for simulation of the flare and touchdown characteristics. The primary piloting task was an instrument approach to a breakout at a 200-ft ceiling with a visual landing. (Author)


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    Titel :

    Fixed Base Simulator Study of an Externally Blown Flap STOL Transport Airplane During Approach and Landing


    Beteiligte:
    W. D. Grantham (Autor:in) / L. T. Nguyen (Autor:in) / J. M. Patton (Autor:in) / P. L. Deal (Autor:in) / R. A. Champine (Autor:in)

    Erscheinungsdatum :

    1972


    Format / Umfang :

    98 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch