To provide data on stability and control characteristics of gliders, flight tests were made over angle of attack range from 10 to 35° with and without artificial pitch and roll damping added; force tests were made from -4 to 40° angle of attack to determine static stability and control characteristics and from 0 to 30° angle of attack to determine dynamic stability derivatives.


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    Titel :

    Investigation of low-subsonic flight characteristics of model of hypersonic boost-glide configuration having 78° delta wing


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Paulson, J.W. (Autor:in) / Shanks, R.E. (Autor:in)


    Erscheinungsdatum :

    1961


    Format / Umfang :

    31 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :