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The Free-Piston Shock Tube

Published online by Cambridge University Press:  07 June 2016

R. J. Stalker
R. J. Stalker*
Affiliation:
Physics Department, Australian National University, Canberra
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Summary

A study of shock tube operation with free-piston compression of the driver gas is presented. It is shown theoretically and experimentally that shock Mach numbers exceeding 30 in air may be obtained with an apparatus of moderate size. The operating limitations imposed by the maximum pressures allowed in the apparatus, by the ratio of the volume of the shock tube to the volume of the compression tube, and by the maximum pressure available for driving the piston are all explored theoretically. The compression process is studied experimentally, and results for three different compression tubes are used to indicate empirical rules for maximising the efficiency of the compression process. Streak photographs of the movement of the luminous gas behind the shock wave in a 1 in diameter shock tube are used to demonstrate the quality of the shock-wave motion produced.

Information

Type
Research Article
Information
Aeronautical Quarterly , Volume 17 , Issue 4 , November 1966, pp. 351 - 370
Copyright
Copyright © Royal Aeronautical Society. 1966

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References

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