Numerical Simulation of Thermal Choking of a Channel during Combustion of a Hydrogen–Air Mixture in a Supersonic Flow
Author:
Publisher
Pleiades Publishing Ltd
Subject
General Physics and Astronomy,Energy Engineering and Power Technology,Fuel Technology,General Chemical Engineering,General Chemistry
Link
https://link.springer.com/content/pdf/10.1134/S0010508223040020.pdf
Reference38 articles.
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2. P. E. Rodi, S. Emami, and C. A. Trexler, “Unsteady Pressure Behavior in a Ramjet/Scramjet Inlet," J. Propul. Power 12, (3), 486–493 (1996); DOI: 10.2514/3.24061.
3. H.-J. Tan, S. Sun, and Z.-L. Yin, “Oscillatory Flows of Rectangular Hypersonic Inlet Unstart Caused by Downstream Mass-Flow Choking," J. Propul. Power 25 (1), 138–147 (2009); DOI: 10.2514/1.37914.
4. H. Do, S. Im, M. G. Mungal, and M. A. Cappelli, “The Influence of Boundary Layers on Supersonic Inlet Flow Unstart Induced by Mass Injection," Exp. Fluids 51, 679–691 (2011). DOI: 10.1007/s00348-011-1077-3.
5. G. Zhao, J. Du, H. Yang, et al., “Effects of Injection on Flame Flashback in Supersonic Crossflow," Aerosp. Sci. Technol. 120, 107226 (2022); DOI: 10.1016/j.ast.2021.107226.
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