Dynamic stability calculations were carried out for longitudinal motion of aircraft with delta wing in supersonic region; parameters which are varied in calculations are Mach number, flight altitude, sweep angle, center of gravity location and wing loading; results, obtained partly with digital and analog computer, are analyzed by means of approximated expressions for frequency and damping of components of disturbed motion.


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    Titel :

    Investigation of dynamic longitudinal stability of delta-winged aircraft at supersonic speeds


    Weitere Titelangaben:

    Amsterdam. Nationaal Lucht- en Ruimtevaartlaboratorium (Nat Aero- and Astronautical Research Inst) -- Reports and Trans TN


    Beteiligte:
    Kalkman, C.M. (Autor:in)


    Erscheinungsdatum :

    1963


    Format / Umfang :

    60 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :