[1] Babinsky, H., Harvey, J. K., Shock Wave-Boundary Layer Interactions, Cambridge University Press, 2011.
[2] Bose, D., Brown, J. L., Prabhu, D. K., Gnoffo, P., Johnston, C. O., Hollis, B., Uncertainty Assessment of Hypersonic Aerothermodynamics Prediction Capability, Journal of Spacecraft and Rockets, 50(1), 2013, pp. 12-18.
[3] DeBonis, J. R., Oberkampf, W. L., Wolf, R. T., Orkwis, P. D., Turner, M. G., Babinsky, H., and Benek, J. A., Assessment of Computational Fluid Dynamics and Experimental Data for Shock Boundary-Layer Interactions, AIAA Journal, 50(4), 2012, pp. 891-903.
[4] Sinha, K., Mahesh, K., Candler, G. V., Modeling Shock-Unsteadiness in Shock/Turbulence Interaction, Physics of Fluids, 15(8), 2003, pp. 2290-2297.
[5] Verma, S. B., Stark, R., Haid, O., Relation Between Shock Unsteadiness and the Origin of Side-Loads Inside a Thrust Optimized Parabolic Rocket Nozzle, Aerospace Science and Technology, 10(6), 2006, pp. 474-483.
[6] Dussauge, J. P., Dupont, P., Debieve, J. F., Unsteadiness in Shock Wave Boundary layer Interactions with Separation, Progress in Aerospace Sciences, 10(2), 2006, pp. 85-91.
[7] Estruch, D., Lawson, N. J., MacManus, D. G., Garry, K. P., Stollery, J. L., Measurement of Shock Wave Unsteadiness using a High-Speed Schlieren System and Digital Image Processing, Review of Scientific Instruments, 79(12), 2008, pp. 126108.
[8] Clemens, N. T., Narayanaswamy, V., Low-Frequency Unsteadiness of Shock Wave/Turbulent Boundary Layer Interactions, Annual Review of Fluid Mechanics, 46, 2014, pp. 469-492.
[9] Bertin, J. J., Hypersonic Aerothermodynamics, AIAA Education Series, AIAA, Washington, DC, 1994.
[10] Anderson, J. D., Hypersonic and High Temperature Gas Dynamics, AIAA, 2006.
[11] Holden, M. S., Wadhams, T. P., A Database of Aerothermal Measurements in Hypersonic. Flow in “Building Block” Experiments for CFD Validation, 41st Aerospace Sciences Meeting and Exhibit, 6-9 July 2003, Reno, Nevada, 2003.
[12] Marvin, J. G., Brown, J. L., Gnoffo, P. A., Experimental Database with Baseline CFD Solutions: 2-D and Axisymmetric Hypersonic Shock-Wave/Turbulent-Boundary-Layer Interactions, NASA/TM–2013–216604, 2013.
[13] Narayanaswamy, V., Raja, L. L., Clemens, N. T., Control of Unsteadiness of a Shock Wave/Turbulent Boundary Layer Interaction by using a Pulsed-Plasma-Jet Actuator, Physics of Fluids, 24(7), 2012, p. 076101.
[14] Delery, J., Marvin, J. G., Shock-Wave Boundary Layer Interactions, edited by E. Reshotko, AGARD No. 280, 1986.
[15] Settles, G. S., Dodson, L. J., Supersonic and Hypersonic Shock/Boundary Layer Interaction Data Base, AIAA Journal, 32(7), 1994, pp. 1337-1383.
[16] Arnal, D., Delery, J. M., Laminar-Turbulent Transition And Shock-Wave/Boundary-Layer Interaction, RTO-EN-AVT-116, Chapter 4, 2004, p. 46.
[17] Ostlund, J., Klingmann, B. M., Supersonic Flow Separation with Application to Rocket Engine Nozzles, AppliedMechanics Reviews, 58, 2005, pp. 143-177.
[18] John, B., Kulkarni, V., Effect of Leading Edge Bluntness on the Interaction of Ramp Induced Shock Wave with Laminar Boundary Layer at Hypersonic Speed, Computers and Fluids, 96, 2014, pp. 177-190.
[19] Sriram , R., Srinath, L., Manoj, K., Devaraj, K., Jagadeesh, G., On the Length Scales of Hypersonic Shock-Induced Large Separation Bubbles Near Leading Edges, Journal of Fluid Mechanics, 806, 2016, pp. 304-355.
[20] Neuenhahm T, Olivier H., Influence of the Wall Temperature and Entropy Layer Effects on Double Wedge Shock Boundary Layer Interactions, 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference, International Space Planes and Hypersonic Systems and Technologies Conferences, 2006-8136, 2006.
[21] Brown, L., Fischer, C., Boyce, R. R., Reinartz, B., Olivier, H., Computational Studies of the Effect of Wall Temperature on Hypersonic Shock-Induced Boundary Layer Separation, Shock Waves, In: Hannemann K., Seiler F. (eds) Shock Waves. Springer, Berlin, Heidelberg, 2009.
[22] Xiaodong, Z., Zhenghong, G., A Numerical Research on a Compressibility-correlated Langtry’s Transition Model for Double Wedge Boundary Layer Flows, Chinese Journal of Aeronautics, 24, 2011, pp. 249-257.
[23] Yang Z., Large-Eddy Simulation: Past, Present and the Future, Chinese Journal of Aeronautics, 28(1), 2015, pp. 11-24.
[24] Knight, D. D., Degrez, G., Shock Wave Turbulent Boundary Layer Interactions In High Mach Number Flows a Critical Survey of Current Numerical Prediction Capabilities, AGARD Advisory Report, 319(2), 1998, pp. 1-35.
[25] Knight, D., Yan, H., Panaras, A. G., Zheltovodov, A., Advances in CFD Prediction of Shock Wave Turbulent Boundary Layer Interactions, Progress in Aerospace Sciences, 39(2-3), 2003, pp. 121-184.
[26] Roy, C. J., Blottner, F. G., Review and Assessment of Turbulence Models for Hypersonic Flows, Progress in Aerospace Sciences, 42(7-8), 2006, pp. 469-530.
[27] Guohua, T. U., Xiaogang, D., Assessment of Two Turbulence Models and Some Compressibility Corrections for Hypersonic Compression Corners by High-Order Difference Schemes, Chinese Journal of Aeronautics, 25, 2012, pp. 25-32.
[28] Rui, Z., Chao, Y., Jian, Y., Xinliang, L., Improvement of Baldwin-Lomax Turbulence Model for Supersonic Complex Flows, Chinese Journal of Aeronautics, 26(3), 2013, pp. 529-534.
[29] Li, M., Lipeng, L. , Jian, F., Qiuhui, W., A Study on Turbulence Transportation and Modification of Spalart-Allmaras Model for Shock-Wave/Turbulent Boundary Layer Interaction Flow, Chinese Journal of Aeronautics, 27(2), 2014, pp. 200-209.
[30] Georgiadis, N. J., Yoder, D. A., Vyas, M. A., Engblom, W. A., Status Of Turbulence Modeling For Hypersonic Propulsion Flow paths, Theoretical and Computational Fluid Dynamics, 28(3), 2014, pp. 295-318.
[31] Panaras, A. G., Turbulence Modeling of Flows with Extensive Cross Flow Separation, Aerospace, 2, 2015, pp. 461-481.
[32] Gaitonde, D. V., Progress in Shock Wave/Boundary Layer Interactions, Progress in Aerospace Sciences, 72, 2015, pp. 80-99.
[33] Elfstrom, G. M., Turbulent Hypersonic Flow at a Wedge- Compression Corner, Journal of Fluid Mechanics, 53(1), 1972, pp. 113-127.
[34] Wilcox, D. C., Turbulence Modeling for CFD, La Canada CA: 2nd edition, DCW Industries, 2000.
[35] Sinha, K., Candler, G. V., Convergence Improvement of Two Equation Turbulence Model Calculations, 29th AIAA, Fluid Dynamics Conference, Fluid Dynamics and Co-located Conferences, Minneapolis, Albuquerque, U.S.A., 1998.
[36] Wilcox, D. C., Formulation of the k-ω Turbulence Model Revisited, AIAA Journal, 46(11), 2008, pp. 2823-2838.
[37] MacCormack, R. W., Candler, G.V., The Solution of Navier-Stokes Equations Using Gauss-Siedal Line Relaxation, Computers and Fluids, 17(1), 1989, pp. 135-150.
[38] Wright, M. J., Candler, G. V., Bose, D., Data-Parallel Line Relaxation Method for the Navier-Stokes Equations, AIAA Journal, 36(9), 1998, pp. 1603-1609.
[39] Sinha, K., Mahesh, K., Candler, G. V., Modeling the Effect of Shock-Unsteadiness in Shock Turbulent Boundary-Layer Interactions, AIAA Journal, 43(3), 2005, pp. 586-594.
[40] Pasha, A. A., Sinha, K., Shock-Unsteadiness Model Applied to Oblique Shock Wave/Turbulent Boundary-Layer Interaction, International Journal of Computational Fluid Dynamics, 22(8), 2008, pp. 569-582.
[41] Pasha, A.A., Sinha, K., Shock Unsteadiness Model Applied to Hypersonic Shock Wave Turbulent Boundary-Layer Interactions, Journal of Propulsion and Power, 28(1), 2012, pp. 46-60.
[42] Menter, F. R., Two-Equation Eddy-Viscosity Turbulence Models for Engineering Applications, AIAA Journal, 32(8), 1994, pp. 1598-1605.