Shock structure in separated nozzle flows
Author:
Publisher
Springer Science and Business Media LLC
Subject
General Physics and Astronomy,Mechanical Engineering
Link
https://link.springer.com/content/pdf/10.1007/s00193-008-0173-7.pdf
Reference20 articles.
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3. Frey M., Hagemann G.: Restricted shock separation in rocket nozzles. J. Propuls. Power 16, 478–484 (2000)
4. Gross A., Weiland C.: Numerical simulation of separated cold gas nozzle flows. J. Propuls. Power 20, 509–519 (2004)
5. Gross A., Weiland C.: Numerical simulation of hot gas nozzle flows. J. Propuls. Power 20, 879–891 (2004)
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