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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    Title :

    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


    Additional title:

    NASA -- Tech Note


    Contributors:
    Gillis, C.L. (author) / Vitale, A.J. (author)


    Publication date :

    1960


    Size :

    42 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :