AIAA Journal · 1966 · 27 citations · 10 references
EngineeringAerospace EngineeringMathematicsAerodynamicsComputational Fluid DynamicsFluid DynamicsComputational AerodynamicsHypersonic AerodynamicsShock WavesSupersonic AerodynamicsBow Shock DynamicsDetached Shock WavesHypersonic FlowShock - Boundary-layer InteractionShock DynamicsShock Wave ModelingSupersonic FlowUnsteady Flow
1 Van Dyke, M., The supersonic blunt-body problem—review and extensions/' J. Aeronaut. Sci. 25, 485-496 (1958). 2 Garabedian, P. R. and Lieberstein, H. M., On the numerical calculation of detached bow shock waves in hypersonic flow, J. Aeronaut. Sci. 25, 109-118 (1958). 3 Swigart, R., Hypersonic blunt-body flowfields at angle of attack, AIAA J. 2, 115-117 (1964). 4 Swenson, E. V., Numerical computation of hypersonic flow past a two-dimensional blunt body, Atomic Energy Commission Research and Development Rept. NYO 1480-1, Courant Institute of Mathematical Sciences, New York Univ. (1964). 5 Bielotserkovskii, O. M., On the calculation of flow past axisymmetric bodies with detached shock waves using an electronic computing machine, Prikl. Mat. Mekh. 24, 511-517 (1960). 6 Prosnak, W. J. and Luczywek, E., The direct asymmetric hypersonic blunt-body problem, AIAA Preprint 64-552 (1964). 7 Bazzhin, A. P., On the computation of the supersonic flow about a flat plate with a detached shock wave, Inzh. Zh. 3, 222227 (1963). 8 Waldman, G. D., Integral approach to the yawed blunt body problem, AIAA Paper 65-28 (1965). 9 Godunov, S. K., Zabrodin, A. O., and Prokopov, G. P., A difference scheme for two-dimensional unsteady flow with a detached shock wave, Zh. Vychyslitelnoi Mat. Mat, Fiz. I, 10201050 (1961); also available as a Cornell Aeronautical Lab. transl. 10 Bohachevsky, I. O. and Rubin, E. L., A direct method for computation of nonequilibrium flows with detached shock waves, AIAA J. 4, 600-607 (1966). 11 Lax, P. D., Weak solutions of nonlinear hyperbolic equations and their numerical computations, Commun. Pure Appl. Math. 7, 159-193 (1954). 12 Kaattari, G. E., Shock envelopes of blunt bodies at large angles of attack, NASA TN D-1980 (December 1963). 13 Vaglio-Laurin, R., Transonic rotational flow over a convex corner, J. Fluid Mech. 9, 81-103 (1960). 14 Kaattari, G. E., Predicted shock envelopes about two types of vehicles at large angles of attack, NASA TN D-860 (April 1961).
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Test Time in Low-Pressure Shock Tubes
Harold Mirels · The Physics of Fluids · 1963 · 340 citations
Shock tube test time limitation due to turbulentwall boundary layer
Harold Mirels · AIAA Journal · 1964 · 237 citations · Full text
Shock-Tube Performance at Low Initial Pressure
Russell E. Duff · The Physics of Fluids · 1959 · 145 citations
On Flow Duration in Low-Pressure Shock Tubes
A. Roshko · The Physics of Fluids · 1960 · 136 citations