Numerical study of the start-up process in an optimized rocket nozzle

Author:

Moríñigo José Antonio,Salvá José Juan

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference17 articles.

1. T. Alziary de Roquefort, Unsteadiness and side loads in over-expanded supersonic nozzles, in: Proc. 4th European Symp. Aerothermodynamics for Space Vehicles, ESA SP-487, Capua, Italy, 2001

2. Numerical investigation of separated nozzle flow;Chen;AIAA J.,1994

3. Unsteady side loads in a thrust-optimized contour nozzle at hysteresis regime;Deck;J. Propulsion and Power,2004

4. Restricted shock separation in rocket nozzles;Frey;J. Propulsion and Power,2000

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

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