Status of flow separation prediction in rocket nozzles

34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 1998, Pages

  Frey, M ^a   Hagemann, G ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

FLOW SEPARATION; FORECASTING; PROPULSION; ROCKETS; WALL FLOW;

AMBIENT PRESSURES; NUMERICAL RESULTS; RECOMPRESSION SHOCKS; REGULAR SHOCK REFLECTIONS; RESTRICTED SHOCK SEPARATION; SEPARATION CRITERION; SHOCK STRUCTURE; THEORETICAL STUDY;

ROCKET NOZZLES;

EID: 85088191896     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-3619     Document Type: Conference Paper

References (21)

1. Summerfield, M., Foster, C., and Swan, W., Flow Separation in Overexpanded Supersonic Exhaust Nozzles, JET PROPULSION, pp. 319 ff., September-October 1954
2. Lawrence, R. A., Symmetrical and Unsymmetrical Flow Separation in Supersonic Nozzles, Ph. D. Thesis, Southern Methodist University, April 1967
3. Schmucker, R., Strömungsvorgänge beim Betrieb überexpandierter Düsen chemischer Raketentrïebwerke (Flow Processes in Overexpanded Nozzles of Chemical Rocket Engines - in German), Report TB-7,-10,-14, Technical University Munich, July 1973
4. Sunley, H. L. G., and Ferriman, D. L. C., Jet Separation in Conical Nozzles, JOURNAL OF THE ROYAL AERONAUTICAL SOCIETY, pp 808-817, Vol. 68, December 1964
5. Nguyen, T. V., and Pieper, J. L., Nozzle Flow Separation, Proceedings of the 5th International Symposium of Propulsion in Space Transportation, France, May 1996
6. Nave, L. H., and Coffey, G. A., Sea Level Side Loads in High-Area-Ratio Rocket Engines, AIAA 73-1284, July 1973
7. Chen, C. L., Chakravarthy, S. R., and Hung, C. M., Numerical Investigation of Separated Nozzle Flows, AIAA JOURNAL, Vol. 32, No. 9, September 1994
8. Stenholm, T., and Jover, V., Flow Separation Control Activities at Volvo and SEP, ESA Advanced Nozzle Workshop, University of Rome, Italy, October 1997
9. Hagemann, G., Schley, C., Odintsov, E., and Sobatchkine, A., Nozzle Flowfield Analysis with Particular Regard to 3D-Plug-Cluster Configurations, AIAA 96-2954, July 1996
10. Hagemann, G., Frey, M., and Manski, D., A Critical Assessment of Dual-Bell Nozzles, AIAA 97-3299, July 1997
11. Nickerson, G., Dang, L., and Coats, D., Two Dimensional Reference Computer Program, NAS 9-12652, MSFC, April 1977
12. Schlichting, H., and Gersten, K., Grenzschicht- Theorie (Boundary Layer Theory - in German), Springer Verlag Berlin Heidelberg, 1997
13. Ahlberg, J. H., Hamilton, S., Migdal, D., and Nilson, E. N., Truncated Perfect Nozzles in Optimum Nozzle Design, ARS JOURNAL, pp. 614-620, May 1961
14. Rao, G. V. R., Exhaust Nozzle Contours for Optimum Thrust, JET PROPULSION, pp. 377-382, June 1958
15. Rao, G. V. R., Approximation of Optimum Thrust Nozzle Contours, ARS JOURNAL, p. 561, June 1960
16. Shapiro, A. H., Compressible Fluid Flow, John Wiley &z Sons New York, 1953
17. 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 - in French), Ph. D. Thesis, University of Rouen, France, January 1997
18. Arens, M., and Spiegler, E., Shock Induced Boundary Layer Separation in Over expanded Conical Exhaust Nozzles, AIAA JOURNAL, Vol. 1, No. 3, March 1963
19. Parley, J. M., and Campbell, C. E., Performance of Several Method-of-Characteristics Exhaust Nozzles, NASA Technical Note D-293, April 1960
20. Girard, S., and Alziary de Roquefort, T., Study of Flow Separation in Over expanded Rocket Nozzles, 4th French-Russian-Italian- Uzbek Workshop, Marseille, France, July 1997
21. Dumnov, G. E., Unsteady Side-Loads Acting on the Nozzle with Developed Separation Zone, AIAA 96-3220, July 1996