References
- Katanoda, H., Miyazato, Y., Masuda, M. and Matsuo, K., 2000, "Pitot Pressures of Correctly-Expanded and Underexpanded Free Jets from Axisymmetric Supersonic Nozzles," Shock Waves, Vol.10, No.3, pp.95-101. https://doi.org/10.1007/s001930050182
- Yuceil, K. B. and Otugen, M. V., 2002, "Scaling Parameters for Underexpanded Supersonic Jets," Physics of Fluids, Vol.14, No.12, pp.4206-4215. https://doi.org/10.1063/1.1513796
- Teshima, K., 1993, "Shock Structure of a Supersonic Free Jet Issuing from a Rectangular Orifice," Proc. Symp. on Shock Waves, Japan' 92, pp.473-476.
- Chpoun, A. and Ben-Dor, G., 1995, "Numerical Confirmation of the Hysteresis Phenomenon in the Regular to the Mach Reflection Transition in Steady Flows," Shock Waves, Vol.5, pp.199-203. https://doi.org/10.1007/BF01419001
- Ben-Dor, G., 1995, "Reconsideration of the State-ofthe-Art of the Shock Wave Reflection Phenomenon in Steady Slows," Jap. Soc. of Mech. Eng., Int. Journal, B, Vol.38, No.3, pp.325-334.
- Ivanov, M. S., Vandromme, D., Fomin, V. M., Kudryavtsev, A. N., Hadjadj, A. and Khotyanovsky, D. V., 2001, "Transition between Regular and Mach Reflection of Shock Waves: New Numerical and Experimental Results," Shock Waves, Vol.11, pp.199-207. https://doi.org/10.1007/PL00004075
-
Ben-Dor, G., Elperin, T., Li, H. and Vasiliev, E., 1997, "Downstream Pressure Induced Hysteresis in the Regular
$\leftrightarrow$ Mach Reflection Transition in Steady Flows," Phys. Fluids, Vol.9, No.10, pp.3096-3098. https://doi.org/10.1063/1.869417 -
Ben-Dor, G., Ivanov, M., Vasilev, E. I. and Elperin, T., 2002, "Hysteresis Processes in the Regular Reflection
$\leftrightarrow$ Mach Reflection Transition in Steady Flows," Progress in Aerospace Sciences, Vol.38, pp.347-387. https://doi.org/10.1016/S0376-0421(02)00009-X - Gribben, B. J., Badcook, K. J. and Richards, B. E., 2000, "Numerical Study of Shock-Reflection Hysteresis in an Underexpanded Jet," AIAA Journal, Vol.38, No.2, pp.275-283. https://doi.org/10.2514/2.954
- Hadjadj, A., 2004, "Numerical Investigation of Shock-Reflection Phenomena in Overexpanded Supersonic Jet," AIAA Journal, Vol.42, No.3, pp.570-577. https://doi.org/10.2514/1.989
- Baig, A., Rizvi, H., Zahir, S. and Khan, M. A., 2005, "Investigation of Shock-Reflection Hysteresis Pheno mena in Supersonic Jet of Overexpanded Flow", Proceedings of the 8th International Symposium on Fluid Control Measurement and Visualization, Chengdu, China, pp.1-9.
- Yasunobu, T., Matsuoka, K., Kashimura, H., Matsuo, S. and Setoguchi, T., 2006, "Numerical Study for Hysteresis Phenomena of Shock Wave Reflection in Overexpanded Axisymmetric Supersonic Jet," Journal of Thermal Science, Vol.15, No.3, pp.220-225. https://doi.org/10.1007/s11630-006-0220-6
- Irie, T., Yasunobu, T., Kashimura, H. and Setoguchi, T., 2004, "Hysteresis Phenomena of Mach Disk Formation in an Underexpanded Jet," Theoretical and Applied Mechanics Japan, Vol.53, pp.181-187.
- Kim, H. D., Kang, M. S., Otobe, Y. and Setoguchi, T., 2009, "The Effect of Nonequilibrium Condensation on Hysteresis Phenomenon of Under-Expanded Jets," Journal of Mechanical Science and Technology, Vol.23, pp.856-867. https://doi.org/10.1007/s12206-009-0207-9
- Al-Hasan, N. S. and Schnerr, G. H., 2007, "Aerodynamic Optimization of Laval Nozzle Flow with Shocks: Numerical Investigation of Active/Passive Shock Control Via Expansion Fans," PAMM Proc. Appl. Math. Mech., 7, 4110003-4110004. https://doi.org/10.1002/pamm.200700222
- Matsuo, K., Miyazato, Y. and Kim, H. D., 1999, "Shock Train and Pseudo-Shock Phenomena in Internal Gas Flows," Progress in Aerospace Sciences, Vol.35, pp.33-100. https://doi.org/10.1016/S0376-0421(98)00011-6
- Menter, F. R., 1993, "Zonal Two Equation k-u Turbulence Models for Aerodynamic Flows," AIAA Paper 93-2906.
- Menter, F. R., 1994, "Two-Equation Eddy-Viscosity Turbulence Models for Engineering Applications," AIAA Journal, Vol.32, pp.269-289.
- Menter, F. R., Kuntz, M. and Langtry, R., 2003, "Ten Years of Industrial Experience with the SST Turbulence Model," Turbulence, Heat and Mass Transfer, 4, pp.625-632.
- Nebbache, A. and Pilinski, C., 2006, "Pulsatory Phenomenon in a Thrust Optimized Contour Nozzle," Aerospace Science and Technology, Vol.10, pp.295-308. https://doi.org/10.1016/j.ast.2005.07.002