Hostname: page-component-cd9895bd7-p9bg8 Total loading time: 0 Render date: 2024-12-22T06:22:04.850Z Has data issue: false hasContentIssue false
  • English
  • Français

Experiments on transition of Mach reflexion

Published online by Cambridge University Press:  29 March 2006

L. F. Henderson  and
A. Lozzi
L. F. Henderson
Affiliation:
Department of Mechanical Engineering, University of Sydney
A. Lozzi
Affiliation:
Department of Mechanical Engineering, University of Sydney
Get access Rights & Permissions [Opens in a new window]

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.

Type
Research Article
Information
Journal of Fluid Mechanics , Volume 68 , Issue 1 , 11 March 1975 , pp. 139 - 155
Copyright
© 1975 Cambridge University Press

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

Bardsley, O. & Mair, Mr. A. 1951 Phil. Mag. 42, 39.
Bleakney, W. & Taub, A. H. 1949 Rev. Mod. Phys. 21, 584.
Chapman, D. R., Keuhn, D. M. & Larson, H. K. 1958 Rep. Nat. Adv. Comm. Aero., Wash. no. 1356.
Eggink, H. 1943 Zentralstelle Wissenshaftliche Ber. (2 WB), Aachen, no. 1850.
Grifbith, W. C. & Bleakney, W. 1954 Am. J. Phys. 22, 597.
Guderley, K. G. 1947 Tech. Rep. Headquarters Air Materiel Command, Wright Field, Dayton, Ohio, F-TR-2168 ND.
Gvozdeava, L. G., Bazhenova, T. V., Predvoditeleva, O. A. & Fokeev, V. P. 1969 Astron. Acta, 14, 503.
Gvozdeava, L. G., Bazhenova, T. V., Predvoditeleva, O. A. & Fokeev, V. P. 1970 Aatron. Acta, 15, 503.
Henderson, L. F. 1964 Aero. Quart. 15, 181.
Henderson, L. F. 1965 Aero. Quart. 16, 42.
Henderson, L. F. 1966 J. Fluid ikfech. 26, 607.
Holder, D. W. & Gadd, G. E. 1955 Boundary Layer Effects in Aerodynamics. London: Her Majesty's Stationery Office.
Jones, D. M., Martin, P. M. E. & Thornhill, C. K. 1951 Proc. Roy. Soc. A 209, 238.
Kawamura, R. & Saito, H. 1956 J. Phys. Soc. Japan, 11, 584.
Landau, L. D. & Lifshitz, E. M. 1959 Fluid Mechanics. Pergamon.
Law, C. K. & Glass, I. I. 1971 C.A.S.I. Trans. 4, 2.
Lean, G. H. 1946 Rep. Aero. Res. Comm. no. 10629 G.B.
Lozzi, A. 1971 Double Mach reflexion of shock waves. M.Eng.Sc. thesis, University of Sydney.
Merritt, D. L. 1968 A.I.B.A. J. 6, 1208.
Mölder, S. 1971 C.A.S.I. Trans. 4, 73.
Neumann, J. VON 1963 Collected Works, vol. 6. Pergamon.
Semenov, A. H., Syshchikova, M. P. & Berezpina, M. K. 1970 Sov. Phys. Tech. Phys. 15, 795.
Smith, L. G. 1945 Photographic investigations of the reflection of plane shocks in air. O.S.R.D. Rep. no. 6271.Google Scholar
Smith, W. R. 1959 Phys. Fluids, 2, 533.
Stanyukovich, K. P. 1960 Unsteady Motion of Continuous Media. Pergamon.
Sternberg, J. 1959 Phys. Fluids, 2, 179.
Wecken, F. 1949 Z. angew. Math. Mech. 29, 147.
Weynantes, R. R. 1968 Tech. Note Inst. Aerospace Studies, University of Toronto, Utias 126.
White, D. R. 1952 Proc. 2nd Mawestern Conj. on Fluid Mech., p. 253. Columbus: Ohio
Wuest, W. 1948 Z. angew. Math. Mech. 28, 3.