Experiments on transition of Mach reflexion
- 11 March 1975
- journal article
- research article
- Published by Cambridge University Press (CUP) in Journal of Fluid Mechanics
- Vol. 68 (01) , 139-155
- https://doi.org/10.1017/s0022112075000730
Abstract
Detailed experimental data are presented on the transition between regular and Mach reflexion. Data have been obtained for steady, pseudo-steady and un-steady flows, and include a study of the continuous and discontinuous transitions predicted by previous researchers. It is found that the criterion often used to calculate the transition condition is wrong in every case that we have investigated. In its place we propose an alternative criterion which has the property that the system remains always in mechanical equilibrium during transition.Keywords
This publication has 10 references indexed in Scilit:
- The refraction of a plane shock wave at a gas interfaceJournal of Fluid Mechanics, 1966
- The Three-Shock Confluence on a Simple Wedge IntakeAeronautical Quarterly, 1965
- On the Confluence of Three Shock Waves in a Perfect GasAeronautical Quarterly, 1964
- Mutual Reflection of Two Shock Waves of Arbitrary StrengthsPhysics of Fluids, 1959
- Triple-Shock-Wave IntersectionsPhysics of Fluids, 1959
- Reflection of Shock Waves–1 Pseudo-Stationary CaseJournal of the Physics Society Japan, 1956
- Shock Waves in GasesAmerican Journal of Physics, 1954
- Interaction of Shock WavesReviews of Modern Physics, 1949
- Grenzlagen gegabelter VerdichtungsstößeZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik, 1949
- Zur Theorie des gegabelten VerdichtungsstoßesZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik, 1948