Numerical simulation of transient flows in a rocket propulsion nozzle-Reference-Cited by-同舟云学术

Numerical simulation of transient flows in a rocket propulsion nozzle

Published:2010-06 Issue:3 Volume:31 Page:409-417
ISSN:0142-727X
Container-title:International Journal of Heat and Fluid Flow
language:en
Short-container-title:International Journal of Heat and Fluid Flow

Author:

Lijo Vincent,Kim Heuy Dong,Setoguchi Toshiaki,Matsuo Shigeru

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference27 articles.

1. Alziary de Roquefort, T., 2001. Unsteadiness and side loads in over-expanded supersonic nozzles. In: Proceedings of the 4th European Symposium on Aerothermodynamics for Space Vehicles (ESA SP-487), Capua, Italy, 15pp.

2. Numerical investigation of separated nozzle flows;Chen;AIAA Journal,1994

3. Frey, M., Hagemann, G., 1998. Status of Flow Separation Prediction in Rocket Nozzles. AIAA Paper 98-3619.

4. Frey, M., Hagemann, G., 1999. Flow separation and side-loads in rocket nozzles. AIAA Journal 99, 2815.

5. Fu, B., Leschziner, M., 1987. Modeling strongly swirling recirculating jet flow with Reynolds-stress transport closures. In: Sixth Symposium on Turbulent Shear Flows, Toulouse, France.

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