Shock pattern in the plume of rocket nozzles: needs for design consideration

Author:

Hagemann Gerald,Frey Manuel

Publisher

Springer Science and Business Media LLC

Subject

General Physics and Astronomy,Mechanical Engineering

Reference13 articles.

1. Hoffman, J.D.: Design of compressed truncated perfect nozzles. AIAA-85–1172 (1985)

2. Rao, G.V.R.: Exhaust Nozzle Contours for Optimum Thrust. Jet Propuls. 28(6), 377–383 (1958)

3. Rao, G.V.R.: Approximation of optimum thrust nozzle contours. ARS J. 30(6), 561 (1960)

4. Moelder, S., Gulamhussein. A., Timofeev, E., Voinovich, P.: Focusing of conical shocks at the centreline of symmetry. In: Proceedings of the 21st International Symposium on Shock Waves (1997)

5. Frey, M.: Behandlung von Strömungsproblemen in Raketendüsen bei Überexpansion. Ph.D. Dissertation, Institute of Aerodynamics and Gasdynamics, University of Stuttgart (2001)

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