References
- Bement, D.A., Stevens, J.R. and Thompson, M.W., "Measured Operation Characteristics of a Rectangular Combustor/Inlet Isolator," AIAA/SAE/ASME/ASEE 26th Joint Propulsion Conference, Orlando, F.L., U.S.A., pp. 90-2221, Jul. 1990.
- Waltrup, P.J. and Billing, F.S., "Structure of Shock Waves in Cylindrical Ducts," AIAA Journal, Vol. 11, No. 10, pp. 1404-1408, 1973. https://doi.org/10.2514/3.50600
- Mitani, T., Chinzei, N. and Kanda, T., "Reaction and Mixing-Controlled Combustion in Scramjet Engines," Journal of Propulsion and Power, Vol. 17, No. 2, pp. 308-314, 2001. https://doi.org/10.2514/2.5743
- Chun, J., Scheuermann, T., von Wolfersdorf, J. and Weigand, B., "Experimental Study on Combustion Mode Transition in a Scramjet with Parallel Injection," 46th AIAA Aerospace Sciences Meeting and Exhibit, Canberra, Australia, AIAA 2006-8063, Nov. 2006.
- Masumoto, R., Tomioka, S., Kudo, K., Murakami, A., Kado, K. and Yamasaki, H., "Experimental Study on Combustion Modes in a Supersonic Combustor," Journal of Propulsion and Power, Vol. 27, No. 2, pp. 346-355, 2011. https://doi.org/10.2514/1.B34020
- Kouchi, T., Masuya, G. and Tomioka, T.M.S., "Mechanism and Control of Combustion-Mode Transition in a Scramjet Engine," Journal of Propulsion and Power, Vol. 28, No. 1, pp. 106-112, 2012. https://doi.org/10.2514/1.B34172
- Fotia, M.L., "Experimental Study of Shock-train/Combustion Coupling and Flame Dynamics in a Heated Supersonic Flow," Michigan University, Ann Arbor, M.I., U.S.A., 2012.
- Curran, E.T. and Murthy, S.N.B., "Scramjet Propulsion," Progress in Astronautics and Aeronautics, Vol. 189, pp. 369-446, 2001.
- Ben-Yakar, A. and Hanson, R.K., "Cavity Flame-holders for Ignition and Flame Stabilization in Scramjets: An Overview," Journal of Propulsion and Power, Vol. 17, No. 4, pp. 869-877, 2001. https://doi.org/10.2514/2.5818
- Matsuo, K., Miyazato, Y. and Kim, H.D., "Shock Train and Pseudo-Shock Phenomena in Internal Gas Flows," Progress in Aerospace Sciences 35, Vol. 35, No. 1, pp. 33-100, Jan. 1999. https://doi.org/10.1016/S0376-0421(98)00011-6
- Shapiro, A.H., The Dynamics and Thermodynamics of Compressible Fluid Flow, The Ronald Press Company, New York, N. Y., U.S.A., pp. 219-260, 1953.
- Heiser, W.H. and Pratt, D.T., Hypersonic Air-breathing Propulsion, AIAA Education Series, Reston, V.A., U.S.A., 1994.
- Micka, D.J. and Driscoll, J.F., "Dual-Mode Combustion of a Jet in Cross-Flow with Cavity Flame-holder," 46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, N.V., U.S.A., AIAA 2008-1062, Jan. 2008.
- Micka, D.J., "Combustion Stabilization, Stucture and Spreading in a Laboratory Dual-Mode Scramjet Combustor," Michigan University, Ann Arbor, M.I., U.S.A., 2010.
- ANSYS. Canonsburg, PA: ANSYS, Inc., ANSYS Fluent 17.0 Theory Guide, 2016.
- Clark, R.J. and Bade Shrestha, S.O., "A Review of Numerical Simulation and Modeling of Combustion in Scramjets," Proceedings of the Institution of Mechanical Engineers, Part G : Journal of Aerospace Engineering, Vol. 229, No. 5, pp. 958-980, 2015. https://doi.org/10.1177/0954410014541249
- Gawehn, T., Gulhan, A., Al-Hasan, N.S. and Schnerr, G.H., "Experimental and Numerical Analysis of the Structure of Pseudo-Shock Systems in Laval Nozzles with Parallel Side Walls," Shock Waves, Vol. 20, No. 4, pp. 297-306, 2010. https://doi.org/10.1007/s00193-010-0263-1
- Bao, W., Yang, Q., Chang, J., Zong, Y. and Hu, J., "Dynamic Characteristics of Combustion Mode Transitions in a Strut-Based Scramjet Combustor Model," Journal of Propulsion and Power, Vol. 29, No. 5, pp. 1244-1248, 2013. https://doi.org/10.2514/1.B34921
- Mitani, T. and Kouchi, T., "Flame Structures and Combustion Efficiency Computed for a Mach 6 Scramjet Engine," Combustion and Flame, Vol. 142, No. 3, pp. 187-196, 2005. https://doi.org/10.1016/j.combustflame.2004.10.004
- Das, R. and Kim, H.D., "Unsteady Flow Characteristics in a Cavity Based Scramjet Combustor," 43th Conference of the Korean Society of Propulsion Engineers, Gangwon-do, Korea, pp. 538-546, Dec. 2014.
- Lee, S.H., "Characteristics of Dual Transverse Injection in Scramjet Combustor, Part: 2: Combustion," Journal of Propulsion and Power, Vol. 22, No. 5, pp. 1020-1026, 2006. https://doi.org/10.2514/1.14185
- Fotia, M.L. and Driscoll, J.F., "Ram-Scram Transition and Flame/Shock-Train Interactions in a Model Scramjet Experiment," Journal of Propulsion and Power, Vol. 29, No. 1, pp. 261-273, 2012. https://doi.org/10.2514/1.B34486
- Fotia, M.L., "Mechanism of Combustion Mode Transition in a Direct-Connect Ramjet-Scramjet Experiment," Journal of Propulsion and Power, Vol. 31, No. 1, pp. 69-78, 2015. https://doi.org/10.2514/1.B35171
- Ikawa, H., "Rapid Methodology for Design and Performance Prediction of Integrated Supersonic Combustion Ramjet Engine," Journal of Propulsion and Power, Vol. 7, No. 3, pp. 437-444, 1991. https://doi.org/10.2514/3.23345
- Bolender, M.A. and Doman, D.B., "Nonlinear Longitudinal Dynamical Model of an Air-Breathing Hypersonic Vehicle," Journal of Spacecraft and Rockets, Vol. 44, No. 2, pp. 374-387, 2007. https://doi.org/10.2514/1.23370
- Torrez, S.M., Scholten, N.A., Micka D.J., Driscoll, J.F., Bolender, M.A., Doman, D.B. and Oppenheimer, M.W., "A Scramjet Engine Model Including Effects of Precombustion Shocks and Dissociation," 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Hartford, C.T., U.S.A., AIAA 2008-4619, Jul. 2008.
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