Effects of nose shape, afterbody shape, fineness ratio, and transition strips are presented at several subsonic Mach numbers through angle of attack range from -- 4 to 24°; applicability to recoverable low lift vehicles capable of atmospheric entry at high speeds.


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    Titel :

    Some effects of nose bluntness and fineness ratio on static longitudinal aerodynamic characteristics of bodies of revolution at subsonic speeds


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:


    Erscheinungsdatum :

    1961


    Format / Umfang :

    65 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :