Pressure signatures of F-100, F-104, and B-58 aircraft at distances from 120 to 425 ft from generating aircraft and at Mach numbers from 1.2 to 1.8 are shown; calculations made by using G.B.Whitham's method gave good agreement with experimental results; procedure for calculating F(y) function used relating to flow field is also given.


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    Titel :

    Experimental and calculated flow fields produced by airplanes flying at supersonic speeds


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Smith, H.J. (Autor:in)


    Erscheinungsdatum :

    1960


    Format / Umfang :

    24 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




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