Numerical calculation of FSS/RSS transition in highly overexpanded rocket nozzle flows
Author:
Publisher
Springer Science and Business Media LLC
Subject
General Physics and Astronomy,Mechanical Engineering
Link
http://link.springer.com/content/pdf/10.1007/s00193-009-0244-4.pdf
Reference28 articles.
1. Frey, M., Hagemann, G.: Status of flow separation prediction in rocket nozzles. AIAA Paper 98-3619 (1998)
2. Nasuti F., Onofri M.: Viscous and inviscid vortex generation during startup of rocket nozzles. AIAA J. 36, 809–815 (1998)
3. Onofri, M., Nasuti, F.: The physical origin of side loads in rocket nozzles. AIAA Paper 99-2587 (1999)
4. Frey, M., Hagemann, G.: Flow separation and side loads in rocket nozzles. AIAA Paper 99-2815 (1999)
5. Reijasse, P., Morzenski, L., Blacodon, D., Birkemeyer, J.: Flow separation experimental analysis in overexpanded subscale rocket-nozzles. AIAA Paper 2001-3556 (2001)
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