A simulation program was conducted to examine specific airworthiness criteria proposed by the STOL Standards Development Working Group. The simulation included an airplane model which was deliberately designed to just meet as many of the proposed criteria as possible. The specific areas of investigation were longitudinal flight path/flight reference control, limiting flight conditions and safety margins, and propulsion system failure. Simulation results largely confirmed the approaches taken by the Working Group and aided in providing additional numerical definition of criteria. (AUthor)


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    Title :

    A Simulator Evaluation of Tentative STOL Airworthiness Criteria. Volume II. Background Information


    Contributors:
    R. K. Heffley (author) / J. M. Lehman (author) / R. L. Stapleford (author) / B. C. Scott (author) / C. S. Hynes (author)

    Publication date :

    1975


    Size :

    79 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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    Airworthiness Considerations for STOL Aircraft

    C. A. Holzhauser / R. C. Innis / H. C. Quigley | NTIS | 1970



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