Numerical simulation of shock-induced separated flows in overexpanded rocket nozzles
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Publisher
EDP Sciences
Link
http://www.eucass-proceedings.eu/10.1051/eucass/201203169/pdf
Cited by 10 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Gas dynamics at starting and terminating phase of a supersonic exhaust diffuser with a conical nozzle;Physics of Fluids;2024-03-01
2. Comparative analysis of 2D simulations and isentropic equations for compressible flow in experimental nozzles;INCAS BULLETIN;2023-09-04
3. Evaluation of generalized k-ω turbulence model in strong separated flow estimation of thrust optimized parabolic nozzle;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2023-08-21
4. Experimental and comprehensive investigation of second throat diffuser area effect on ground test of a thrust optimized parabolic nozzle with different expansion ratios;Acta Astronautica;2023-08
5. Starting transient analysis of second throat exhaust diffuser in high-altitude test of a thrust optimized parabolic nozzle;Physics of Fluids;2023-06-01
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