Numerical study on the shock transitions during off-design operation of a dual throat thruster
Author:
Publisher
Springer Science and Business Media LLC
Subject
General Physics and Astronomy,Mechanical Engineering
Link
https://link.springer.com/content/pdf/10.1007/s00193-021-01037-3.pdf
Reference24 articles.
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3. Hagemann, G., Immich, H., Nguyen, T.V., Dumnov, G.E.: Advanced rocket nozzles. J. Propuls. Power 14(5), 620–634 (1998). https://doi.org/10.2514/2.5354
4. Lundgreen, R., Nickerson, G., O’Brien, C.: Dual throat thruster cold flow analysis. ALRC Report F 32666 (1978)
5. Ben-Dor, G., Ivanov, M., Vasilev, E., Elperin, T.: Hysteresis processes in the regular reflection $$\leftrightarrow $$ Mach reflection transition in steady flows. Prog. Aerosp. Sci. 38(4–5), 347–387 (2002). https://doi.org/10.1016/S0376-0421(02)00009-X
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