Abstract
The influence of an incoming boundary layer to the standing morphology of an oblique detonation wave (ODW) induced by a compression ramp is numerically studied in this paper. The Spalart-Allmaras (SA) turbulence model is used to perform simulation of detonationboundary- layer interactions. Three different wall conditions are applied to realize control on the boundary-layer separation scales. Accordingly, different standing morphologies of the ODWs are obtained, including smooth ODW (without transverse wave) under no-slip, adiabatic wall condition with large-scale separation, abrupt ODW (with transverse wave) under no-slip, cold wall condition with moderate-scale separation, and bow-shaped detached ODW under slipwall condition without a boundary layer.
References
[1] F. W. Spaid, J. L. Frishett, AIAA J. 10, 915 (1972)10.2514/3.50245Search in Google Scholar
[2] G. S. Settles, S. M. Bogdonoff, I. E. Vas, AIAA J. 14, 50 (1976)10.2514/3.61331Search in Google Scholar
[3] G. S. Settles, T. J. Fitzpatrick, S. M. Bogdonoff, AIAA J. 17, 579 (1979)10.2514/3.61180Search in Google Scholar
[4] J. Green, Prog. Aerospace Sci. 11, 235 (1970)10.1016/0376-0421(70)90018-7Search in Google Scholar
[5] E.E. Zhukoski, AIAA J. 5, 1746 (1967)10.2514/3.4299Search in Google Scholar
[6] R.H. Korkegi, AIAA J. 13, 534 (1975)10.2514/3.49750Search in Google Scholar
[7] M. S. Holden, AIAA 10th Aerospace Sciences Meeting, No.72-74, January 17-19, 1972, San Diego, California, USASearch in Google Scholar
[8] K. J. Plotkin, AIAA J. 13, 1036-1040 (1975)10.2514/3.60501Search in Google Scholar
[9] B. Ganapathisubramani, N. T. Clemens, D. S. Dolling, J. Flui. Mech. 585, 369- (2007)10.1017/S0022112007006799Search in Google Scholar
[10] J. Fay, Phys. Fluids 2, 283 (1959)10.1063/1.1705924Search in Google Scholar
[11] E. K. Dabora, J. A. Nicholls, R. B. Morrison, Proc. Combust. Inst. 10, 817 (1965)10.1016/S0082-0784(65)80225-9Search in Google Scholar
[12] S. B.Murray, Ph.D. thesis, McGill University (Montreal, Canada, 1984)Search in Google Scholar
[13] W. P. Sommers, R. B. Morrison, Phys. Fluids 5, 241 (1962)10.1063/1.1706602Search in Google Scholar
[14] S. B. Murray, J. H. Lee, Prog. Astronaut. Areonaut. 106, 329 (1986)Search in Google Scholar
[15] C. Li, K. Kailasanath, E. S. Oran, 31st Aerospace Sciences Meeting and Exhibit, No.93-0450, January 11-14, 1993, Reno, NV, USASearch in Google Scholar
[16] J. Y. Choi, I. S. Jeung, Y. Yoon, Proc. Combust. Inst. 2181 (1998)10.1016/S0082-0784(98)80067-2Search in Google Scholar
[17] F.Giovanni, Ph.D. thesis, University of Toronto (Toronto, Canada, 2003)Search in Google Scholar
[18] D. T. Pratt, J.W. Humphrey, D. E. Glenn, J.Propulsion 7, 837 (1991)10.2514/3.23399Search in Google Scholar
[19] L. Figueira Da Silva, B. Deshaies, Combust.Flame 121, 152 (2000)10.1016/S0010-2180(99)00141-8Search in Google Scholar
[20] A. F. Wang, W. Zhao, Z. L. Jiang, Acta Mech. 27, 611 (2011)10.1007/s10409-011-0463-7Search in Google Scholar
[21] H. H. Teng, Z. L. Jiang, J.Fluid Mech. 713, 659 2012)10.1017/jfm.2012.478Search in Google Scholar
[22] P. R. Spalart, S. R. Allmaras, AIAA J. 94 (1992)Search in Google Scholar
[23] N. Peters, Turbulent combustion, 3rd edition (Cambridge university press, Cambridge, 2000)Search in Google Scholar
[24] P. L. Roe, Annual Review of Fluid Mechanics, 18, 337 (1986)10.1146/annurev.fl.18.010186.002005Search in Google Scholar
[25] D. S. Dolling, M. T. Murphy, AIAA J. 21, 1628 (1983) 10.2514/3.60163Search in Google Scholar
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