Numerical Analysis of Flow Separation in Rocket Nozzles
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Publisher
Springer India
Link
http://link.springer.com/content/pdf/10.1007/978-81-322-2743-4_117
Reference7 articles.
1. Hegab, A.M., Kassoy, D.R., Sileem, A.A.: Numerical investigation of acoustic-fluid dynamics interaction in an SRM chamber/nozzle model. In: 36th Aerospace Science Meeting, Reno, NV, USA, AIAA Paper 98-0712 (1998)
2. Östlund, J., Bigert, M.: A Subscale investigation on side-loads in sea level rocket nozzles. In: 35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA Paper 99-2759, June 1999
3. Östlund, J., Jaran, M.: Assessment of turbulence models in overexpanded rocket nozzle flow simulations. In: 35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA Paper 99-2583, June 1999
4. Allamaprabhu, C.Y., Raghunandan, B.N., Morinigo, J.A.: Improved prediction of flow separation in thrust optimized parabolic nozzles with FLUENT. In: 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA 2011–5689 (2011)
5. Xu, J., Zhao, C.: Two-dimensional numerical simulations of shock waves in micro convergent–divergent nozzles. In: International Journal of Heat and Mass Transfer 50 2434–2438 (2007)
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1. Nozzle Flow Separation Phenomena and Control for different conditions;3;2022-12-01
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