Hostname: page-component-586b7cd67f-vdxz6 Total loading time: 0 Render date: 2024-11-29T10:03:26.111Z Has data issue: false hasContentIssue false

Analysis of a piston-driven shock tube

Published online by Cambridge University Press:  04 July 2016

Gabi Ben-Dor
Affiliation:
Department of Mechanical Engineering, Ben-Gurion University of the Negev, Israel
Ozer Igra
Affiliation:
Department of Mechanical Engineering, Ben-Gurion University of the Negev, Israel

Extract

A shock tube is a facility that produces fast and A relatively high temperature flows by driving a strong shock wave into quiescent gas. From simple shock tube theory it is possible to show that in order to obtain high Mach number primary shock waves one should employ a very light driving gas at the highest pressure and temperature possible. These conditions are most commonly met by the explosion of a stochiometric mixture of inflammable gases, such as oxygen and hydrogen diluted with helium.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1978 

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

1. Glass, I. I. and Hall, J. G. Handbook of supersonic aerodynamics. Section 18, Shock Tubes. NAVORD Report 1488, Vol 6, 1959.Google Scholar
2. Ben-dor, G. and Igra, O. Design study of a piston driven shock tube. Polytechnic Institute of New York, Department of Aerospace Engineering and Applied Mechanics, Report No 76-5, September 1976. (See also Ben-Gurion University of the Negev, Department of Mechanical Engineering Report No 9/76, 1976, in Hebrew.)Google Scholar
3. Jenkins, R. C. Shock tube operation using a compression heating driver gas. Grumman Research Department, Report No RE-481, 1974.Google Scholar
4. Russell, D. A. A study of area change near the diaphragm of a shock tube. Guggenheim Aeronautical Laboratory, California Institute of Technology, Pasadena, 1960.Google Scholar
5. Stalker, R. J. Characteristics of a free-piston shock tube. Proceedings of the Fifth Shock Tube Symposium, 1965.Google Scholar