Hostname: page-component-586b7cd67f-dlnhk Total loading time: 0 Render date: 2024-11-25T01:44:34.881Z Has data issue: false hasContentIssue false
  • English
  • Français

On the Impingement of Supersonic Jet on a Normal Flat Surface

Published online by Cambridge University Press:  07 June 2016

B.N. Pamadi
B.N. Pamadi*
Affiliation:
Department of Aeronautical Engineering, Indian Institute of Technology, Bombay
Get access

Summary

An improved method, based on one strip approximation of the method of integral relations which was reported originally by Belov, Ginzburg and Shub, is presented for the calculation of flow parameters in the impingement region of a supersonic, underexpanded jet striking a normal surface located within the first cell. The results are presented for two impingement conditions and found to be in good agreement with the experimental data.

Type
Research Article
Information
Aeronautical Quarterly , Volume 33 , Issue 3 , August 1982 , pp. 199 - 218
Copyright
Copyright © Royal Aeronautical Society. 1982

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 Vick, A.R. and Andrews, E.H. Jr. An investigation of highly underexpanded exhaust plumes impinging upon a perpendicular flat surface. NASA TN D-3269, 1966.Google Scholar
2 Land, N.S. and Clark, L.V. Experimental investigation of jet impingement on surfaces of fine particles in vacuum environment. NASA TN D-2633, 1965.Google Scholar
3 Stitt, L.E. Interactions of highly under expanded jets with simulated lunar surfaces. NASA TN D-1095, 1961.Google Scholar
4 Henderson, L.F. Experiments on the impingement of a supersonic jet on a flat plate. Z. Angew. Math. Phys. Vol. 17, pp 553-569, 1966.Google Scholar
5 Gummer, J.H. and Hunt, B.L. The impingement of nonuniform, axisymmetric, supersonic jets on a perpendicular flat plate. Israel Journal of Technology, Vol. 12, pp 221-235, 1974.Google Scholar
6 Carling, J.C. and Hunt, B.L. The near wall jet of a normally impinging, uniform, axisymmetric, supersonic jet. Journal of Fluid Mechanics, Vol. 66, Part 1, pp 159-176, 1974.Google Scholar
7 Lamont, P.J. and Hunt, B.L. The impingement of under expanded jets on wedges. Journal of Fluid Mechanics, Vol. 76, Part 2, pp 307-336, 1976.CrossRefGoogle Scholar
8 Kalaghatgi, G.T. and Hunt, B.L. The occurrence of stagnation bubbles in supersonic jet impingement flows. The Aeronautical Quarterly, Vol. XXVII, pp 169-185, August 1976.Google Scholar
9 Golubkov, A.G., Kozmenko, B.K., Ostapenko, V.A. and Solotchin, A.V. On the interaction of an underexpanded supersonic jet with a finite flat baffle. Fluid Mechanics, Soviet Research, Vol. 3, pp 96-102, 1974.Google Scholar
10 Ginzburg, I.P., Belov, I.A. Zazimko, B.A. and Terpigoreev, B.C. Influence of turbulence on heat transfer of supersonic jet with flat obstacle. Heat and Mass Transfer, Vol. 1, pp 381-393, BSSR Academy of Sciences, Energia, Moscow, 1968.Google Scholar
11 Gummer, J.H. and Hunt, B.L. The impingement of uniform, axisymmetric, supersonic jet on a perpendicular flat plate, Report No. BLH/7001, July 1970, University of Bristol, U.K. Google Scholar
12 Rao, K.S., Purohit, S.C. and Sarma, M.S. Numerical study of nonuniform axisymmetric under expanded supersonic jet impingement on a finite surface. Aeronautical Journal, Vol. 80, pp 313-317, July 1976.Google Scholar
13 Saxena, S.K. Upper stage jet impingement on separated booster. Aeronautical Journal, Vol. 83, pp 71-74, February 1979.Google Scholar
14 Zien, T.F., Chien, K.V. and Driftmyer, R.T. Two dimensional supersonic jet impingement on a flat plate. AIAA Journal, Vol. 17, No. 1, pp 4-5, 1979.CrossRefGoogle Scholar
15 Belov, I.A., Ginzburg, I.P. and Snub, L.I. Supersonic under expanded jet impingement upon flat plate. International Journal of Heat and Mass Transfer, Vol. 16, pp 2067-2076, 1973.CrossRefGoogle Scholar
16 Kalaghatgi, G.T. Some aspects of supersonic jet impingement on a plane perpendicular surfaces. Ph.D. thesis, University of Bristol, 1975.Google Scholar
17 Xerikos, J. and Anderson, W.A. A critical study of the direct blunt body integral method. Douglas Aircraft Corporation, Santa Monica Division, Report No. SM-42603, 1962.Google Scholar
18 Love, E.S., Grigsby, C.E., Lee, L.P. and Woodling, M.J. Experimental and theoretical studies of axisymmetrical free jets. NASA TR R-6, 1959.Google Scholar
19 Ginzburg, I.P. and Sokolov, B.N. Aerodynamics and heat transfer in jet flows (in Russian). Heat and Mass Transfer, Vol. 1, pp 344-357, BSSR, Academy of Sciences, Energia, Moscow, 1968.Google Scholar
20 Kalaghatgi, G.T. and Hunt, B.L. The three shock confluence problem for the case of normally impinging, over expanded jets. The Aeronautical Quarterly, Vol. XXVI, pp 117-132, 1975.CrossRefGoogle Scholar
21 Henderson, L.F. On the confluence of three shock waves in a perfect gas. The Aeronautical Quarterly, Vol. XV, pp 181-197, 1964.Google Scholar
22 Hunt, B.L. An attempted improvement of the method of integral relations for a blunt body in supersonic flow, Rep. No. BLH/7301, April 1973, university of Bristol, U.K. CrossRefGoogle Scholar