Numerical study of restricted shock separation in a compressed truncated perfect nozzle

AIAA Journal

Volumn 44, Issue 3, 2006, Pages 576-584

  Shimizu, Taro ^a,b   Miyajima, Hiroshi ^a,b   Kodera, Masatoshi ^a,c  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b Japan Aerospace Exploration Agency   (Japan)

^c Institute of Space Technology and Aeronautics   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

FLOW STRUCTURE; NONAXISYMMETRIC UNSTEADY FLOW; PARABOLIC NOZZLE; SHOCK SEPARATION;

COMPRESSIBLE FLOW; NAVIER STOKES EQUATIONS; NOZZLES; NUMERICAL ANALYSIS; SEPARATION; UNSTEADY FLOW;

FLOW OF FLUIDS;

EID: 33645398574     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.14288     Document Type: Conference Paper

References (26)

1. Zucrow, M. J., and Hoffman, J. D., Gas Dynamics, Vol. 2, Wiley, New York, 1977, pp. 160-164.
2. Rao, G. V. R., "Exhaust Nozzle Contour for Optimum Thrust," Jet Propulsion, Vol. 28, No. 6, 1958, pp. 377-382.
3. Hoffman, J. D., "Design of Compressed Truncated Perfect Nozzles," Journal of Propulsion, Vol. 3, No. 2, 1987, pp. 150-156.
4. Nave, L. H., and Coffey, G. A., "Sea Level Side Loads in High-Area-Ratio Rocket Engines," AIAA Paper 73-1284, Nov. 1973.
5. Frey, M., and Hagemann, G., "Restricted Shock Separation in Rocket Nozzles," Journal of Propulsion and Power, Vol. 16, No. 3, 2000, pp. 478-484.
6. Hagemann, G., Frey, M., and Koschel, W., "Appearance of Restricted Shock Separation in Rocket Nozzles," Journal of Propulsion and Power, Vol. 18, No. 3, 2002, pp. 577-584.
7. Östlund, J., Damgaard, T., and Frey, M., "Side-Load Phenomena in Highly Overexpanded Rocket Nozzles," Journal of Propulsion and Power, Vol. 20, No. 4, 2004, pp. 695-704.
8. Onofri, M., and Nasuti, F., "The Physical Origins of Side Loads in Rocket Nozzles," AIAA Paper 99-2587, June 1999.
9. Deck, S., and Guillen, P., "Numerical Simulations of Side Loads in an Ideal Truncated Nozzle," Journal of Propulsion and Power, Vol. 18, No. 2, 2002, pp. 261-269.
10. Verma, S. B., "Study of Flow Separation in Truncated Ideal Contour Nozzle," Journal of Propulsion and Power, Vol. 18, No. 5, 2002, pp. 1112-1121.
11. Gross, A., Haidn, O., Stark, R., Zeiss, W., Weber, C., and Weiland, C., "Experimental and Numerical Investigation of Heat Loads in Separated Nozzle Flow," AIAA Paper 2001-3682. July 2001.
12. Gross, A., and Weiland, C., "Numerical Simulation of Separated Cold Gas Nozzle Flows," Journal of Propulsion and Power, Vol. 20, No. 3, 2004, pp. 509-519.
13. Deck, S., and Nguyen, A. T., "Unsteady Side Loads in a Thrust-Optimized Contour Nozzle at Hysteresis Resime," AIAA Journal, Vol. 42, No. 9, 2004, pp. 1878-1888.
14. Wang, T.-S., "Transient Three-Dimensional Analysis of Side Load in Liquid Rocket Engine Nozzles," AIAA Paper 2004-3681, July 2004.
15. Watanabe, Y., and Tsuboi, M., "LE-7A Engine Nozzle Problems During Transient Operations," AIAA Paper 2002-3841, July 2002.
16. Tomita, T., Sakamoto, H., Takahashi, M., Sasaki, M., Tamura, T., and Tsuboi, M., "Sub-Scale Nozzle Combustion Tests of the LE-7A Engine for Clarification of Large Side-Loads (1): Formation of RSS Structure Due to Combustion Condition," AIAA Paper 2002-3842, July 2002.
17. Tomita, T., Sakamoto, H., Onodera, T., Sasaki, M., Takahashi, M., Tamura, H., and Watanabe, Y., "Experimental Evaluation of Side-Load Characteristics on TP, CTP and TO Nozzles," AIAA Paper 2004-3678, July 2004.
18. Yonezawa, K., Yokota, K., Tsujimoto, Y., Sakazume, N., and Watanabe, Y., "Three-Dimensional Unsteady Flow Simulation of Compressed Truncated Perfect Nozzles," AIAA Paper 2002-3991, July 2002.
19. Takahashi, M., Ueda, S., Tomita, T., Takahashi, M., Tamura, H., and Aoki, K., "Transient Flow Simulation of a Compressed Truncated Perfect Nozzle," AIAA Paper 2001-3681, July 2001.
20. Nasuti, F., and Onofri, M., "Viscous and Inviscid Vortex Generation During Startup of Rocket Nozzles," AIAA Journal, Vol. 36, No. 5, 1998, pp. 809-815.
21. Chen, C. L., Chakravarthy, S. R., and Hung, C. M., "Numerical Investigation of Separated Nozzle Flows," AIAA Journal, Vol. 32, No. 9, 1994, pp. 1836-1843.
22. Kodera, M., Sunami, T., and Nakahashi, K., "Numerical Analysis of SCRAMJET Combusting Flows by Unstructured Hybrid Grid Method," AIAA Paper 2000-0886, Jan. 2000.
23. Goldberg, U. C., and Ramakrishnan, S. V., "A Pointwise Version of Baldein-Barth Turbulence Model," Computational Fluid Dynamics, Vol. 1, No. 4, 1993, pp. 321-338.
24. Venkatakrishnan, V., "On the Accuracy of Limiters and Convergence to Steady State Solutions," AIAA Paper 93-0880, Jan. 1993.
25. Kano, S., Yamamoto, S., and Daiguji, H., "An Efficient CFD Approach for Simulating Unsteady Hypersonic Shock-Shock Interference Flows," Computers and Fluids, Vol. 27, Nos. 5-6, 1998, pp. 571-580.
26. Lovely, D., and Haimes, R., "Shock Detection from Computational Fluid Dynamics Results," AIAA Paper 99-3285, July 1999.