Effects of lift were real and significant; measured bow-shock intensities agreed fairly well with, but were consistently less than, shock intensities estimated by theoretical methods; available flight data were examined for correlation with wind tunnel test results.


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    Titel :

    Investigation of influence of lift on sonic-boom intensity by means of wind-tunnel measurements of pressure fields of several wing-body combinations at mach number of 2.01


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Carlson, H.W. (Autor:in)


    Erscheinungsdatum :

    1961


    Format / Umfang :

    37 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :