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.
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
NASA -- Tech Note
1961
37 pages
Article (Journal)
English
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