Investigation was conducted in Langley 4- by 4-ft supersonic pressure tunnel; 5 models were tested with fineness ratios varying from 19.1 to 14.8; tests covered angle-of-attack range up to about 28° for complete configuration and various combinations of component parts.


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    Titel :

    Aerodynamic characteristics in pitch of series of cruciform-wing missiles with canard controls at mach number of 2.01


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Spearman, M.L. (Autor:in)


    Erscheinungsdatum :

    1961


    Format / Umfang :

    40 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :