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A Note on Shock Detachment Distance

Published online by Cambridge University Press:  04 July 2016

J. L. Stollery  and
D. J. Maull
J. L. Stollery
Affiliation:
Aeronautics Department, Imperial College of Science and Technology
D. J. Maull
Affiliation:
Aeronautics Department, Imperial College of Science and Technology
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Extract

There have been numerous attempts to predict the stand—off distance of bow shock waves, ranging from the exact solutions of the inviscid flow equations by Mangier (1959) and Van Dyke (1959) to the semi—empirical treatment of Moeckel (1949) and Love (1957). Sinnott (1959) has recently proposed a single formula Δ/R=K cot θm where K is a numerical constant given as 0·77 for axisymmetric bodies and the symbols are defined in Fig. 1.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 64 , Issue 594 , June 1960 , pp. 357 - 359
Copyright
Copyright © Royal Aeronautical Society 1960

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References

1.Boison, J. C. and Curtiss, H. A. (1959). An experimental investigation of blunt body stagnation point velocity gradient. A.R.S. Journal, Vol. 29, No. 2, February 1959.Google Scholar
2.Lees, L. (1957). Recent developments in hypersonic flow. Jet Propulsion, Vol. 27, No. 11, November 1957.CrossRefGoogle Scholar
3.Love, E. S. A re–examination of the use of simple concepts for predicting the shape and location of detached shock waves. N.A.C.A. T.N. 4170.Google Scholar
4.Mangler, K. W. (1957-9). The calculation of the flow field between a blunt body and the bow wave. Paper presented at the Colston Symposium on Hypersonic Flow, Bristol, April 1959. See also R.A.E. Tech. Note Aero 2536, October 1957.Google Scholar
5.Moeckel, W. E. (1949). Approximate method for predicting form and location of detached shock waves ahead of plane or axially symmetric bodies. N.A.C.A. T.N. 1921,1949.Google Scholar
6.Serbin, H. (1958). The high speed flow of gas around blunt bodies. Aeronautical Quarterly, Vol. IX, Nov. 1958.Google Scholar
7.Sinnott, C. S. An analysis of shock detachment distance in supersonic flow. A.R.C. 21,078.Google Scholar
8.Van Dyke, M. D. and Gordon, Helen D. (1959). Super-sonic flow past a family of blunt axisymmetric bodies. N.A.S.A. Tech. Report R-l, 1959.Google Scholar
9.Warren, C. H. E. (1956.) Recent Advances in the Knowledge of Transonic Air Flow. Journal of the Royal Aeronautical Society, Vol. 60. April 1956.CrossRefGoogle Scholar