A WIND-TUNNEL INVESTIGATION AT A MACH NUMBER OF 2.01 OF THE SONIC-BOOM CHARACTERISTICS OF THREE WING-BODY COMBINATIONS DIFFERING IN WING LONGITUDINAL LOCATION
Wind tunnel tests on sonic boom with models of three wing-fuselage combinations
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Wind tunnel tests on sonic boom with models of three wing-fuselage combinations
Dependence of sonic boom overpressures on supersonic aircraft configurations and design aspects to minimize boom
Atmospheric effects on sonic boom pressure wave shapes
Effect of aircraft configuration on sonic boom overpressures
Ground measurement of sonic boom pressure for fighter and bomber aircraft at stratospheric altitudes
Wind tunnel and flight testing of airplane configuration influence on sonic boom characteristics
Correlation of sonic boom theory with wind tunnel and flight measurements
Sonic boom ground overpressure measurements in Oklahoma
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