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Application of the minimum entropy production principle to shock reflection induced by separation

Published online by Cambridge University Press:  26 October 2018

Chengpeng Wang*
Affiliation:
College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, PR China
Longsheng Xue
Affiliation:
College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, PR China
Keming Cheng
Affiliation:
College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, PR China
*
Email address for correspondence: [email protected]

Abstract

In this paper separation-induced shock reflection is studied theoretically and experimentally. An analytical model is proposed to establish the connections among upstream conditions, downstream conditions and shock configurations. Furthermore, the minimum entropy production principle is employed to determine the incident shock angles as well as the criterion for the transition from regular reflection to Mach reflection, which agrees well with experimental results. Additionally, a solution path for a reflected shock that fulfills the minimum entropy production principle is found in the overall regular reflection domain, based on which the steadiest shock configuration may be determined according to upstream and downstream conditions.

Type
JFM Papers
Copyright
© 2018 Cambridge University Press 

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References

Azevedo, D. J. & Liu, C. S. 1993 Engineering approach to the prediction of shock patterns in bounded high-speed flows. AIAA J. 31, 8390.Google Scholar
Bai, C. Y. & Wu, Z. N. 2017 Size and shape of shock waves and slip line for Mach reflection in steady flow. J. Fluid Mech. 818, 116140.Google Scholar
Ben-Dor, G. 1991 Shock Wave Reflection Phenomena. Springer.Google Scholar
Chapman, D. R., Kuehn, D. M. & Larson, H. K.1958 Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition. NACA Tech. Rep. 1356.Google Scholar
Chpoun, A., Passerel, D., Li, H. & Ben-Dor, G. 1995 Reconsideration of oblique shock wave reflections in steady flows. Part 1. Experimental investigation. J. Fluid Mech. 301, 1935.Google Scholar
Crocco, L. 1958 One-dimensional treatment of steady gas dynamics. In Fundamentals of Gas Dynamics (ed. Emmons, H. W.), pp. 110130. Princeton University Press.Google Scholar
Délery, J. & Marvin, J. G.1986 Shock-wave boundary layer interactions. Tech. Rep. 280. AGARD.Google Scholar
Gao, B. & Wu, Z. N. 2010 A study of the flow structure for Mach reflection in steady supersonic flow. J. Fluid Mech. 656, 2950.Google Scholar
Glansdorff, P. & Prigogine, A. 1971 Thermodynamic Theory of Structure Stability and Fluctuations. Wiley.Google Scholar
Hornung, H. G., Oertel, H. & Sandeman, R. J. 1979 Transition to Mach reflection of shockwaves in steady and pseudo-steady flow with and without relaxation. J. Fluid Mech. 90, 541547.Google Scholar
Hornung, H. G. & Robinson, M. L. 1982 Transition from regular to Mach reflection of shock waves. Part 2. The steady-flow criterion. J. Fluid Mech. 123, 155164.Google Scholar
Hu, Z. M., Myong, R. S., Kim, M. S. & Cho, T. H. 2009 Downstream flow condition effects on the RR→MR transition of asymmetric shock waves in steady flows. J. Fluid Mech. 620, 4362.Google Scholar
Ivanov, M. S. I., Ben-Dor, G., Elperin, E., Kudryavtes, A. N. & Khotyanovsky, D. V. 2002 The reflection of asymmetric shock waves in steady flows: a numerical investigation. J. Fluid Mech. 469, 7187.Google Scholar
Kawamura, R. & Satto, H. 1956 Reflection of shock waves – 1. Pseudo-stationary case. J. Phys. Soc. Japan. 11, 584592.Google Scholar
Li, H. & Ben-Dor, G. 1996a Application of the principle of minimum entropy production to shock wave reflection. Part I. Steady flow. J. Appl. Phys. 80, 20272037.Google Scholar
Li, H. & Ben-Dor, G. 1996b Application of the principle of minimum entropy production to shock wave reflection. Part II. Unsteady flow. J. Appl. Phys. 80, 20382048.Google Scholar
Li, H., Chpoun, A. & Ben-Dor, G. 1999 Analytical and experimental investigations of the reflection of asymmetric shock waves in steady flows. J. Fluid Mech. 390, 2543.Google Scholar
Mach, E. 1878 Uber den verlauf von funkenwellen in der ebeneund im raume. Sitzugsbr. Akad. Wiss. Wien. 78, 819838.Google Scholar
Matsuo, K., Miyazato, Y. & Kim, H. D. 1999 Shock train and pseudo-shock phenomena in internal gas flows. Prog. Aeronaut. Sci. 35, 33100.Google Scholar
von Neumann, J.1943 Oblique reflection of shocks. Tech. Rep. 12. Navy Department, Bureau of Ordnance, Washington DC.Google Scholar
von Neumann, J.1945 Refraction, intersection and reflection of shock waves. Tech. Rep. 203. Navy Department, Bureau of Ordnance, Washington DC.Google Scholar
Tao, Y., Fan, X. Q. & Zhao, Y. L. 2014 Viscous effects of shock refection hysteresis in steady supersonic flows. J. Fluid Mech. 759, 134148.Google Scholar
Tao, Y., Liu, W. D., Fan, X. Q., Xiong, B., Yu, J. F. & Sun, M. B. 2017 A study of the asymmetric shock reflection configurations in steady flows. J. Fluid Mech. 825, 115.Google Scholar
Wang, C. P., Xue, L. S. & Tian, X. A. 2017 Experimental characteristics of oblique shock train upstream propagation. Chin. J. Aeronautics. 30, 663676.Google Scholar
Wang, Z. G., Zhao, Y. L., Zhao, Y. X. & Fan, X. Q. 2015 Prediction of massive separation of unstarted inlet via free-interaction theory. AIAA J. 53, 11031111.Google Scholar
Xue, L. S., Wang, C. P. & Cheng, K. M. 2018 Dynamic characteristics of separation shock in an unstarted hypersonic inlet flow. AIAA J. 56, 24842490.Google Scholar