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The choked jet flowing into a stationary atmosphere

Published online by Cambridge University Press:  04 July 2016

J. C. Gibbings
J. C. Gibbings*
Affiliation:
Fluid Mechanics Division, University of Liverpool
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Extract

A previous discussion of the expanding flow of a choked axi-symmetric jet into a stationary atmosphere drew attention to the differences between various existing sets of observations and between observation and analysis. One reason advanced for these discrepancies was the influence of the mixing region at the edge of the jet while another was the degree of uniformity and steadiness of the flow at exit from the nozzle.

Type
Technical note
Information
The Aeronautical Journal , Volume 79 , Issue 776 , August 1975 , pp. 368 - 370
Copyright
Copyright © Royal Aeronautical Society 1975 

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References

1. Gibbings, J. C., Ingham, J. and Johnson, D. Flow in a supersonic jet expanding from a convergent nozzle. ARC Current Paper 1197, 1972.Google Scholar
2. Kurn, A. G. Experiments with a jet close to a plane surface (RAE report to be published.)Google Scholar
3. Love, E. S., Grisby, C. E., Lee, L. P. and Woodling, M. J. Experimental and theoretical studies of axi-symmetric free jets. NASA TR R-6, 1959.Google Scholar
4. Young, C. A theoretical investigation of supersonic jets in subsonic flow fields. ARC Current Paper 1256, 1973.Google Scholar
5. Frandtl, L. von. Uber die stationaren Wellen in einem Gasstrahl. Physikalische Zeitschrift Vol 5, p 599, 1904.Google Scholar
6. Stow, P. The interaction of a sonic jet with a surround ing subsonic stream. The Aeronautical Quarterly Vol 25, p 232, August 1974.Google Scholar
7. Pack, D. C. A note on Prandtl's formula for the wavelength of a supersonic gas jet. Quart Jour Mech and App Maths, Vol 3, Pt 2, p 173. 1950.Google Scholar
8. Courant, R. and Friedrichs, K. O. Supersonic flow and shock waves. Interscience, New York, p 392, 416, 1948.Google Scholar
9. Sloan, D. The displacement of the nose shock wave from a pitot-tube under a stream-wise velocity gradient. The Aeronautical Journal, Vol 71, No 682, p 725, October 1967.Google Scholar
10. Simmons, G. A. Effect of nozzle boundary-layers on rocket exhaust plumes. AlAA Journal, Vol 10, Pt 11, p 1534, November 1972.Google Scholar
11. Chirivella, J. and Kuby, W. C. Semi-empirical calculations of the interaction of a slightly under expanded jet with a quiescent atmosphere. Journal of Spacecraft Vol 7, Pt 7, p 871, July 1970. ,Google Scholar