A simulator study of short takeoff and landing (STOL) aircraft was conducted using a model of a deflected slipstream transport aircraft. The subjects considered are: (1) the approach, (2) flare and landing, (3) go-around, and (4) takeoff phases of flight. The results are summarized and possible implications with regard to airworthiness criteria are discussed. A data base is provided for future STOL airworthiness requirements and a preliminary indication of potential problem areas is developed. Comparison of the simulation results with various proposed STOL criteria indicates significant deficiencies in many of these criteria.


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    Titel :

    A STOL airworthiness investigation using a simulation of a deflected slipstream transport. Volume 1: Summary of results and airworthiness implications


    Beteiligte:
    Stapleford, R. L. (Autor:in) / Heffley, R. K. (Autor:in) / Rumold, R. C. (Autor:in) / Hynes, C. S. (Autor:in) / Scott, B. C. (Autor:in)

    Erscheinungsdatum :

    1974-10-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






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