Characteristics of trim, drag, pitch damping, and longitudinal stability are presented; theoretical comparisons of lift and longitudinal stability and experimental results from similar configuration are included.


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    Title :

    Aerodynamic characteristics over mach number range of 1.40 to 2.78 of rocket propelled airplane configuration having low 52.5° delta wing and unswept horizontal tail


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1961


    Size :

    26 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :