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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    Title :

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


    Additional title:

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


    Contributors:


    Publication date :

    1963


    Size :

    60 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :