This paper will present the scope of an NASA program aimed at improving the design and evaluation techniques relative to stall/spin characteristics of general-aviation aircraft. The program encompasses analytical studies, full-scale and model wind-tunnel tests, radio-control model, and full-scale flight tests. Initial spin-tunnel results of several tail designs on a representative light airplane will be discussed.


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    Title :

    Stall/Spin Research Status Report


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    National Business Aircraft Meeting and Engineering Display ; 1974



    Publication date :

    1974-02-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English