Study made to determine transonic and supersonic longitudinal stability, control and drag characteristics of aircraft and missile configurations; from results obtained total effects of wing can be determined; for some of aerodynamic derivatives separate effects of wing, tail, and fuselage were determined.


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    Titel :

    Wing-on and wing-off longitudinal characteristics of airplane configuration having thin unswept wing of aspect ratio 3, as obtained from rocket-propelled models at mach numbers from 0.8 to 1.4


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Gillis, C.L. (Autor:in) / Vitale, A.J. (Autor:in)


    Erscheinungsdatum :

    1960


    Format / Umfang :

    42 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :