AIAA Journal · 1978 · 44 citations · 14 references
Natural SciencesAerospace EngineeringPhysicsAerodynamicsComputational Fluid DynamicsFluid DynamicsInviscid FlowShock WavesOblique Shock WavesOblique Wave ReflectionShock - Boundary-layer InteractionShock Tube FlowShock Wave DynamicsShock Wave-boundary Layer InteractionShock-boundary Layer InteractionShock-wave Reflection
Oblique shock-wave reflections in nitrogen for perfect and imperfect gases were investigated interferometrically in a 10x 18-cm shock tube. Comparisons are made with numerical experiments conducted by two different groups on regular and single-Mach reflections. Even though the analyses are for inviscid flows, the sidewall boundary-layer effects in the experiments are negligible, and the features of the calculated and actual inviscid flows are compared readily. It is found that the available numerical techniques will have to be modified or new approaches developed before acceptable agreement can be obtained between actual and numerical experiments. The very accurate interferometric data will provide a basis for comparison with future numerical methods, which also should include the two remaining cases of complexand double-Mach reflections as a test of their accuracy and applicability.
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Walker Bleakney, A. H. Taub · Reviews of Modern Physics · 1949 · 207 citations
Experiments on transition of Mach reflexion
L. F. Henderson, A Lozzi · Journal of Fluid Mechanics · 1975 · 131 citations