An investigation was conducted at the request of the U.S. Air Force Avionics Laboratory to analyze the flight characteristics of a small uncontrolled glider with folding wings. The study consisted of wind-tunnel tests of an actual glider and a theoretical analysis of the performance, stability, and trimmability of the configuration.


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    Titel :

    Analysis of the Flight Motions of a Small Deployable Glider Configuration


    Beteiligte:
    P. L. Coe (Autor:in)

    Erscheinungsdatum :

    1975


    Format / Umfang :

    32 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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