Flow separation experimental analysis in overexpanded subscale rocket-nozzles

37th Joint Propulsion Conference and Exhibit

Volumn , Issue , 2001, Pages

  Reijasse, Ph ^a   Morzenski, L ^a   Blacodon, D ^a   Birkemeyer, J ^a  

^a ONERA   (France)

Author keywords

[No Author keywords available]

Indexed keywords

PROPULSION; ROCKET NOZZLES; ROCKETS; SHOCK WAVES; WALL FLOW; WIND TUNNELS;

ANALYSIS OF MEANS; AXISYMMETRIC NOZZLES; COMPRESSION RAMPS; EXPERIMENTAL ANALYSIS; NOZZLE PRESSURE RATIO; PRESSURE FLUCTUATION; SHOCK-WAVE/BOUNDARY LAYER INTERACTIONS; WALL PRESSURE MEASUREMENT;

FLOW SEPARATION;

EID: 85085778176     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-3556     Document Type: Conference Paper

References (16)

1. Hagemann, G. and Reijasse, P., "Brief Review of Side-Load Models", Onera report RT44/4361 DAFE/Y; also published as DLR report DLR-IB 645-98/36, December 1998.
2. Hagemann, G., Terhardt, M., Frey, M., Reijasse, P., Onofri, M., Nasuti, F. and Ostlund, J. Flow Separation and Side-Loads in Rocket Nozzles", 4th International Symposium on Liquid Space Propulsion, Lampoldshausen, Germany, March 13- 15, 2000.
3. Frey, M. and Hagemann, G., "Flow Separation and Side-Loads in Rocket Nozzles", AIAA 99-2815, 1999.
4. Terhardt, M., Hagemann, G., and Frey, M., "Flow Separation and Side-Load Behaviour of the Vulcain Engine", AIAA 99-2762, 1999.
5. Mattsson, J., Hogman, U., and Torngren, L., "A Sub-Scale Test Programme on Investigation of Flow Separation and Side-Loads in Rocket Nozzles, Proceedings of the 3rd European Symposium on Aerothermodynamics of Space Vehicles, ESAESTEC, Netherlands, November 24-26, 1998.
6. Ostlund, J. and Bigert, M., "A Subscale Investigation on Side-Loads in Sea Level Rocket Nozzles", AIAA 99-2759, June 1999.
7. Reijasse, P., Servel, P. and Hallard, R., "Synthesis of the 1998-1999 ONERA Works in the FSCD Working Group", ONERA RTS 49/4361 DAFE/Y, December 1999.
8. Reijasse, P. and Morzenski, L. "Campagne de mesure de charges laterales dans des tuyeres surdetendues. Soufflerie R2Ch. Programme FSCD" (Test campaign of side load measurements in overexpanded nozzles. R2Ch wind tunnel. FSCD program, in French), Onera report RTS 58/00145 DAFE, November 2000.
9. Takayama, K. and Ben-Dor, G., "The Inverse Mach Reflection", AIAA journal, Vol. 23, No. 12, December 1985.
10. Li, H., Chpoun, A. and Ben-Dor, G., "Analytical and Experimental Investigations of the Reflection of Asymmetric Shock Waves in Steady Flows", J. Fluid Mech.y Vol. 390, pp. 25-43 (1999).
11. Carriere, P., " Remarques sur les Methodes de Calcul des Effets de la Viscosite dans les Tuyeres Propulsives" (Comments on computational methods of viscous effects in propulsion nozzles, in French), DGRR/WGLR Symposium, Bad Godesberg, also published as ONERA TP 408, October 1966.
12. Delery, J., and Marvin J.G., "Shock-Wave Boundary Layer Interactions", AGARD No. 280, February 1986.
13. Schmucker, R., "Flow Processes in Overexpanding Nozzles of Chemical Rocket Engines" (published in German), Report TB-7,-10,- 14, Technical University Munich, 1973.
14. Dolling, D.S. and Or, C.T., "Unsteadiness of the Shock Wave Structure in Attached and Separated Compression Ramp Flow Fields", AIAA 83-1715, July 1983.
15. Muck, K., Dussauge, J.-P. and Bogdonoff, M., "Structure of the Wall Pressure Fluctuations in a Shock-Induced Separated Turbulent Flow", AIAA 85-0179, January 1999.
16. Barter, J.W. and Dolling, D.S., "Reduction of Ructuating Pressure Loads in Shock Wave Turbulent Boundary Layer Interactions", AIAA 95-0673, January 1995.