Restricted Shock Separation in Rocket Nozzles

Journal of Propulsion and Power

Volumn 16, Issue 3, 2000, Pages 478-484

  Frey, Manuel ^a   Hagemann, Gerald ^b  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

^b DAIMLER AG   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0000470279     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.5593     Document Type: Article

References (19)

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4. Campbell, C. E., and Farley, J. M., "Performance of Several Conical Convergent-Divergent Rocket-Type Exhaust Nozzles," NASA TN D-467, May 1960.
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13. Frey, M., and Hagemann, G., "Status of Flow Separation Prediction in Rocket Nozzles," AIAA Paper 98-3619, July 1998.
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15. Shapiro, A. H., Compressible Fluid Flow, Wiley, New York, 1953, pp. 556, 557.
16. Hadjadj, A., "Analyse Physique et Simulation Numerique des Ecoulements Compressibles - Application Aux Tuyeres de Propulseurs (Physical Analysis and Numerical Simulation of Compressible Flows - Application to Rocket Nozzles)," Ph.D. Dissertation, Faculté des Sciences, Univ. of Rouen, France, Jan. 1997.
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19. Dumnov, G. E., "Unsteady Side-Loads Acting on the Nozzle with Developed Separation Zone," AIAA Paper 96-3220, July 1996.