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A holographic interferometry study of an axisymmetric shock-wave/boundary-layer strong interaction flow
(University of Missouri--Columbia, 1986)
pressures of 1.7 and 3.4 atm provided Reynolds number values of 18 • 106 and 36 • 106 based on model length. Three cone angles (12.5°, 20°, and 30°) were studied giving negligible, incipient, and large scale flow separation respectively. The initial cylinder...