Hostname: page-component-848d4c4894-xm8r8 Total loading time: 0 Render date: 2024-07-01T20:40:55.008Z Has data issue: false hasContentIssue false

Shock attenuation by a single transverse slit

Published online by Cambridge University Press:  11 April 2006

J. H. S. Lee
Affiliation:
Department of Mechanical Engineering, McGill University, Montreal, Canada
P. P. Ostrowski
Affiliation:
Department of Mechanical Engineering, McGill University, Montreal, Canada Present address: Department of Mechanical Engineering, University of Maryland, College Park, Md.
J. H. T. Wu
Affiliation:
Department of Mechanical Engineering, McGill University, Montreal, Canada

Abstract

Attenuation of a plane shock due to the interaction with a single slit is examined via spark schlieren photography for shock Mach numbers between 1·17 and 2·44 and slit widths between 0·173 and 3·175 cm. Wave speed measurements by piezoelectric transducers indicate that the attenuation is weak and adequately predicted by Whitham's ray-shock theory. The slit width is observed to produce only a secondary effect on the shock attenuation rate. Stability of the attenuating shock is demonstrated from a wave diagram constructed by the ray-shock technique.

Type
Research Article
Copyright
© 1976 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

Lapworth, K. C. 1959 An experimental investigation of the stability of plane shock waves. J. Fluid Mech. 6, 469.Google Scholar
Milton, B. E. 1971 Shock wave motion and focusing in area contractions. Ph.D. thesis, University of New South Wales, Australia.
Milton, B. E. 1975 Mach reflection using ray-shock theory. A.I.A.A. J. 13, 1531.Google Scholar
Oshima, K., Sugaya, K., Yamamoto, M. & Totoki, T. 1965 Diffraction of a plane shock around a corner. Inst. Space Aero. Sci., Univ. Tokyo, Rep. no. 393.Google Scholar
Skews, B. W. 1972 The shape of a shock wave in regular reflection from a wedge. Can. Aero. & Space Inst. Trans. 5, 28.Google Scholar
Whitham, G. B. 1957 A new approach to problems of shock wave dynamics. Part 1. Two-dimensional problems. J. Fluid Mech. 2, 145.Google Scholar
Whitham, G. B. 1958 On the propagation of shock waves through regions of non-uniform area or flow. J. Fluid Mech. 4, 337.Google Scholar