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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    Title :

    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


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1961


    Size :

    37 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :