Computational Analysis of Effect of Injection Angles in Strut Based Scramjet Combustor
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Publisher
Springer International Publishing
Link
https://link.springer.com/content/pdf/10.1007/978-3-031-67241-5_15
Reference17 articles.
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2. Gerdroodbary, M.B., Ganji, D.D., Amini, Y.: Numerical study of shock wave interaction on transverse jets through multiport injector arrays in supersonic crossflow. Acta Astronaut. 115, 422–433 (2015)
3. Ben-Yakar, A., Hanson, R.K.: Cavity flame-holders for ignition and flame stabilization in scramjets: an overview. J. Propuls. Power 17(4), 869–877 (2001). https://doi.org/10.2514/2.5818
4. Liu, S.J., Pan, Y., Liu, W.D.: Experimental study on the combustion and flow process in a scramjet with strut injector. Hangkong Dongli Xuebao/J. Aerosp. Power 24(1), 55–59 (2009). https://doi.org/10.1016/j.ast.2023.108300
5. Liu, C., Zhang, J., Jia, D., Li, P.: Experimental and numerical investigation of the transition progress of strut-induced wakes in the supersonic flows. Aerosp. Sci. Technol. 120, 107256 (2022). https://doi.org/10.1016/j.ast.2021.107256
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