Flame Interaction Characteristics in Scramjet Combustor Equipped with Strut/Wall Combined Fuel Injectors

References

• Bagg, M., and R. Greendyke (2009). Computational analysis of strut induced mixing in a scramjet. 47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Orlando, FL. (p. 1253).
   Google Scholar
• Bao, W., J. Hu, Y. Zong, Q. Yang, M. Wu, J. Chang, and D. Yu. 2013. Combustion characteristic using O2-pilot strut in a liquid-kerosene-fueled strut-based dual-mode scramjet. Proc. Inst. Mech. Eng. G 227 (12):1870–80. doi:10.1177/0954410012464455.
   Web of Science ®Google Scholar
• Bao, W., Y. Zong, J. Chang, J. Hu, Q. Yang, J. Song, and M. Wu. 2014. Effects of upstream strut on the combustion of liquid kerosene in a model cavity scramjet. Proc. Inst. Mech. Eng. G 228 (12):2323–28. doi:10.1177/0954410013515370.
   Web of Science ®Google Scholar
• Betelin, V. B., N. N. Smirnov, V. F. Nikitin, V. R. Dushin, A. G. Kushnirenko, and V. A. Nerchenko. 2012. Evaporation and ignition of droplets in combustion chambers modeling and simulation. Acta Astronaut. 70:23–35. doi:10.1016/j.actaastro.2011.06.021.
   Web of Science ®Google Scholar
• Candon, M. J., and H. Ogawa. 2018. Numerical analysis and design optimization of supersonic after-burning with strut fuel injectors for scramjet engines. Acta Astronaut. 147:281–96. doi:10.1016/j.actaastro.2018.04.012.
   Web of Science ®Google Scholar
• Chang, J. T., J. L. Zhang, W. Bao, and D. R. Yu. 2018. Research progress on strut-equipped supersonic combustors for scramjet application. Prog. Aerosp. Sci. 103:1–30. doi:10.1016/j.paerosci.2018.10.002.
   Web of Science ®Google Scholar
• Chang, X., H. Gu, and L. Chen (2005). Thrust and drag of a scramjet model with different combustor geometries. AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference, Capua, Italy. (p. 3315).
   Google Scholar
• Curran, E. T. 2001. Scramjet engines: The first forty years. J. Propul. Power 17 (6):1138–48. doi:10.2514/2.5875.
   Web of Science ®Google Scholar
• Feng, S., J. Chang, J. Zhang, C. Zhang, and W. Bao. 2017. Numerical and experimental investigation of improving combustion performance of variable geometry dual-mode combustor. Aerosp. Sci. Technol. 64:213–22. doi:10.1016/j.ast.2017.02.002.
   Web of Science ®Google Scholar
• Hsu, K. Y., C. Carter, M. Gruber, and C. J. Tam (2009). Mixing study of strut injectors in supersonic flows. 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Denver, CO. (p. 5226).
   Google Scholar
• Hsu, K. Y., C. D. Carter, M. R. Gruber, T. Barhorst, and S. Smith. 2010. Experimental study of cavity-strut combustion in supersonic flow. J. Propul. Power 26 (6):1237–46. doi:10.2514/1.45767.
   Web of Science ®Google Scholar
• Hu, J., J. Chang, W. Bao, Q. Yang, and J. Wen. 2014. Experimental study of a flush wall scramjet combustor equipped with strut/wall fuel injection. Acta Astronaut. 104 (1):84–90. doi:10.1016/j.actaastro.2014.07.012.
   Web of Science ®Google Scholar
• Hu, J., J. Qin, J. Chang, W. Bao, Y. Zong, and Q. Yang. 2013. Combustion stabilization based on a center flame strut in a liquid kerosene fueled supersonic combustor. J. Therm. Sci. 22 (5):497–504. doi:10.1007/s11630-013-0654-6.
   Web of Science ®Google Scholar
• Huang, W., and L. Yan. 2016. Numerical investigation on the ram–Scram transition mechanism in a strut-based dual-mode scramjet combustor. Int. J. Hydrogen Energy 41 (8):4799–807. doi:10.1016/j.ijhydene.2016.01.062.
   Web of Science ®Google Scholar
• Kodera, M., T. Sunami, and F. Sheel (2002). Numerical study on the supersonic mixing enhancement using streamwise vortices. AIAA/AAAF 11th International Space Planes and Hypersonic Systems and Technologies Conference, Orleans, France. (p. 5117).
   Google Scholar
• Li, J., R. Jin, G. Jiao, and W. Song. 2018a. Analysis on mode transition in a dual-mode scramjet combustor. Combust. Sci. Technol. 190 (1):82–96. doi:10.1080/00102202.2017.1376190.
   Web of Science ®Google Scholar
• Li, M., X. He, Y. Zhao, Y. Jin, Z. Ge, and W. Huang. 2018b. Effect of strut length on combustion performance of a trapped vortex combustor. Aerosp. Sci. Technol. 76:204–16. doi:10.1016/j.ast.2018.02.019.
   Web of Science ®Google Scholar
• Nishioka, M. 1995. Some thoughts and experiments on the supersonic mixing enhancement. J. Soci. Fluid Mech. 14:377–89.
   Google Scholar
• Pandey, K. M., S. Roga, and G. Choubey. 2015. Computational analysis of hypersonic combustor using strut injector at flight mach 7. Combust. Sci. Technol. 187 (9):1392–407. doi:10.1080/00102202.2015.1035371.
   Web of Science ®Google Scholar
• Sathiyamoorthy, K., T. H. Danish, J. Srinivas, and P. Manjunath. 2018. Experimental investigation of supersonic combustion in a strut-cavity based combustor. Acta Astronaut. 148:285–93. doi:10.1016/j.actaastro.2018.05.014.
   Web of Science ®Google Scholar
• Sun, M. B., H. Geng, J. H. Liang, and Z. G. Wang. 2008. Flame characteristics in supersonic combustor with hydrogen injection upstream of cavity flameholder. J. Propul. Power 24 (4):688–96. doi:10.2514/1.34970.
   Web of Science ®Google Scholar
• Sunami, T., P. Magre, A. Bresson, F. Grisch, M. Orain, and M. Kodera (2005, May). Experimental study of strut injectors in a supersonic combustor using OH-PLIF. AIAA/CIRA 13th International Space Planes And Hypersonics Systems and Technologies Conference, Capua, Italy. (p. 3304).
   Google Scholar
• Sunami, T., A. Murakami, K. Kudo, M. Kodera, and M. Nishioka (2002). Mixing and combustion control strategies for efficient scramjet operation in wide range of flight mach number. AIAA/AAAF 11th International Space Planes and Hypersonic Systems and Technologies Conference, Orleans, France. (p. 5116).
   Google Scholar
• Sunami, T., and F. Scheel (2002). Analysis of mixing enhancement using streamwise vortices in a supersonic combustor by application of laser diagnostics. AIAA/AAAF 11th International Space Planes and Hypersonic Systems And Technologies Conference, Orleans, France. (p. 5203).
   Google Scholar
• Townend, L. H. 2001. Domain of the Scramjet. J. Propul. Power 17 (6):1205–13. doi:10.2514/2.5865.
   Web of Science ®Google Scholar
• Van Driest, E. R. 1951. Turbulent boundary layer in compressible fluids. J. Aircraft. Sci 18 (3):145–60. doi:10.2514/8.1895.
   Web of Science ®Google Scholar
• Vishwakarma, M., and A. Vaidyanathan. 2016. Experimental study of mixing enhancement using pylon in supersonic flow. Acta Astronaut. 118:21–32. doi:10.1016/j.actaastro.2015.09.011.
   Web of Science ®Google Scholar
• Wang, H., Z. Wang, M. Sun, and H. Wu. 2013. Combustion modes of hydrogen jet combustion in a cavity-based supersonic combustor. Int. J. Hydrogen Energy 38 (27):12078–89. doi:10.1016/j.ijhydene.2013.06.132.
   Web of Science ®Google Scholar
• Wang, Y., W. Song, D. Shi, Q. Fu, and Y. Wang. 2017. Experimental study of vitiation effects on combustion characteristics of a supersonic combustor. Combust. Sci. Technol. 189 (9):1500–09. doi:10.1080/00102202.2017.1305368.
   Web of Science ®Google Scholar
• Wang, Z. G., M. B. Sun, H. B. Wang, J. F. Yu, J. H. Liang, and F. C. Zhuang. 2015. Mixing-related low frequency oscillation of combustion in an ethylene-fueled supersonic combustor. Proc. Combust. Inst. 35 (2):2137–44. doi:10.1016/j.proci.2014.09.005.
   Web of Science ®Google Scholar
• Wu, K., P. Zhang, W. Yao, and X. Fan. 2017. Numerical investigation on flame stabilization in DLR hydrogen supersonic combustor with strut injection. Combust. Sci. Technol. 189 (12):2154–79. doi:10.1080/00102202.2017.1365847.
   Web of Science ®Google Scholar
• Zhang, J., J. Chang, J. Ma, Y. Wang, and W. Bao. 2019. Investigations on flame liftoff characteristics in liquid-kerosene fueled supersonic combustor equipped with thin strut. Aerosp. Sci. Technol. 84:686–97. doi:10.1016/j.ast.2018.11.017.
   Web of Science ®Google Scholar
• Zhang, J., J. Chang, J. Ma, C. Zhang, and W. Bao. 2017. Investigation of flame establishment and stabilization mechanism in a kerosene fueled supersonic combustor equipped with a thin strut. Aerosp. Sci. Technol. 70:152–60. doi:10.1016/j.ast.2017.08.005.
   Web of Science ®Google Scholar
• Zhang, J., J. Chang, J. Ma, Y. Zhang, and W. Bao. 2018. Local and global flame characteristics in a liquid kerosene fueled supersonic combustor equipped with a thin strut. Aerosp. Sci. Technol. 76:49–57. doi:10.1016/j.ast.2018.02.007.
   Web of Science ®Google Scholar
• Zhu, S., X. Xu, and P. Ji. 2016. Flame stabilization and propagation in dual-mode scramjet with staged-strut injectors. Aiaa J. 55 (1):171–79. doi:10.2514/1.J054974.
   Google Scholar
• Zhu, S., X. Xu, Q. Yang, and Y. Jin. 2018. Intermittent back-flash phenomenon of supersonic combustion in the staged-strut scramjet engine. Aerosp. Sci. Technol. 79:70–74. doi:10.1016/j.ast.2018.05.037.
   Web of Science ®Google Scholar
• Zhu, S. H., and X. Xu. 2017. Experimental study on flame transition in a two-stage struts dual-mode scramjet. J. Aerosp. Eng. 30 (5):06017002. doi:10.1061/(ASCE)AS.1943-5525.0000740.
   Web of Science ®Google Scholar
• Zong, Y., W. Bao, J. Chang, J. Hu, Q. Yang, J. Song, and M. Wu. 2013. Effect of fuel injection allocation on the combustion characteristics of a cavity-strut model scramjet. J. Aerosp. Eng. 28 (1):04014050. doi:10.1061/(ASCE)AS.1943-5525.0000374.
   Web of Science ®Google Scholar
• Zuo, J., S. Zhang, J. Qin, W. Bao, and N. Cui. 2018. Performance evaluation of regenerative cooling/film cooling for hydrocarbon fueled scramjet engine. Acta Astronaut. 148:57–68. doi:10.1016/j.actaastro.2018.04.037.
   Web of Science ®Google Scholar