Journal of the Korean Society of Propulsion Engineers ISSN:1226-6027(Print) 2288-4548(Online) 한국추진공학회지

Urzay, J., “Supersonic combustion in air-breathing propulsion systems for hypersonic flight,” Annual Review of Fluid Mechanics, Vol. 50, No. 1, 2018, pp. 593–627.

Zettervall, N., and Fureby, C., “A computational study of ramjet, scramjet and dual-mode ramjet combustion in combustor with a cavity flameholder,” 56th AIAA Aerospace Sciences Meeting, Kissimmee, USA, pp. 1146, Jan 2018.

Tian, Y., Xiao, B., Zhang, S., and Xing, J., “Experimental and computational study on combustion performance of a kerosene fueled dual-mode scramjet engine,” Aerospace Science and Technology, Vol. 46, 2015, pp. 451–458.

Lee, G. S., “A combined cycle approach to dual-mode scramjet design and analysis,” Ph.D. Dissertation, Department of Aerospace Engineering, University of Illinois Urbana-Champaign, Urbana, IL, USA, 2023.

Muylaert, J., Kumar, A., Drummond, P., Bouchez, M., McClinton, C. R., Maurice, L. Q., and Hendrick, P., “Technologies for propelled hypersonic flight, Volume 2–Subgroup 2: Scram propulsion,” Technical Report No. TRAVT007V2, 2006.

Dessornes, O., and Scherrer, D., “Tests of the JAPHAR dual mode ramjet engine,” Aerospace Science and Technology, Vol. 9, No. 3, 2005, pp. 211–221.

Vlasenko, V., Voloshchenko, O., Sabelnikov, V., and Talyzin, V., “Choice of geometry and operating regimes for experimental dual-mode high-speed propane-fueled combustion chamber.” AIP Conference Proceedings, Vol. 1893, No. 1, 2017, pp. 2-12.

Li, H. G., Khare, P., Sung, H. G., and Yang, V., “A large-eddy-simulation study of combustion dynamics of bluff-body stabilized flames,” Combustion Science and Technology, Vol. 188, No. 6, 2016, pp. 924–952.

Stechman, R., and Allen, R., “History of ramjet propulsion development at the Marquardt company-1944 to 1970,” 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Tuscon, USA, pp. 3538, Jul 2005.

Webster, F., and Bucy, J., “ASALM-PTV chin inlet technology overview: Advanced Strategic Air Launched Missile Propulsion Technology Validation of integral rocket/ramjet,” 15th Joint Propulsion Conference, Las Vegas, USA, pp. 1240, Jun 1979.

Scherrer, D., Dessornes, O., Ferrier, M., Vincent-Randonnier, A., Moule, Y., and Sabel’nikov, V., “Research on supersonic combustion and scramjet combustors at ONERA,” Journal of Aerospace Lab, No. 11, 2016, pp. 2-21.

Roquemore, W. M., Shouse, D., Burrus, D., Johnson, A., Cooper, C., Duncan, B., Hsu, K.-Y., Katta, V. R., Sturgess, G. J., and Vihinen, I., “Vortex combustor concept for gas turbine engines,” 39th Aerospace Sciences Meeting and Exhibit, Reno, USA, pp. 483, Jan 2001.

Zhao, D., Gutmark, E., and de Goey, P., “A review of cavity-based trapped vortex, ultra-compact, high-g, inter-turbine combustors,” Progress in Energy and Combustion Science, Vol. 66, 2018, pp. 42–82.

Chen, S., “Numerical study of trapped vortex combustors characteristics in small ramjets,” Ph.D. Dissertation, School of Mechanical and Aerospace Engineering, Nanyang Technological University, Singapore, 2016.