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International Journal of Aerospace Engineering
Volume 2017, Article ID 4768376, 13 pages
Research Article

Three-Dimensional Numerical Analysis of LOX/Kerosene Engine Exhaust Plume Flow Field Characteristics

Department of Space Equipment, Equipment Academy, Beijing 101416, China

Correspondence should be addressed to Wan-sheng Nie; moc.621@9691swn

Received 28 November 2016; Accepted 1 August 2017; Published 5 November 2017

Academic Editor: Wen Bao

Copyright © 2017 Hong-hua Cai et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

Linked References

  1. G. Terry, S. David, and P. Robert, “Analysis of liquid rocket propellant engine exhaust plumes,” in AIAA 5th Thermophysics conference, Los Angeles, CA, USA, June 29–July 1, 1970.
  2. D. R. Gonzalez, P. Walman, M. Sanford, J. Monat, and J. Carney, “Characterization of rocket-plume fluid-dynamic environment using numerical and experimental approaches,” Journal of Spacecraft and Rockets, vol. 50, no. 3, pp. 527–539, 2013. View at Publisher · View at Google Scholar · View at Scopus
  3. G. P. Sutton and O. Biblarz, Rocket propulsion elements, John Wiley & Sons, New York, NY, USA, 7th edition, 2001.
  4. F. S. Simmons, Rocket Exhaust Plume Phenomenology, The Aerospace Press, AIAA, Reston, VA, USA, 1st edition, 2000.
  5. A. Mathur, “Rocket plume attenuation model,” in 24th AIAA International Communications Satellite Conference, San Diego, CA, USA, June 2006.
  6. H. William and J. Calhoon, “Computational assessment of afterburning cessation mechanisms in fuel-rich rocket exhaust plumes,” Journal of Propulsion and Power, vol. 17, no. 1, pp. 111–119, 2001. View at Publisher · View at Google Scholar
  7. G. Marshall, H. Jeffrey, and K. Cetin, “Best practices for CFD simulations of launch vehicle ascent with plumes – OVERFLOW perspective,” in 49th AIAA Aerospace Science Meeting including the New Horizons Forum and Aerospace Exposition, Orlando, FL, USA, January 2011.
  8. S.-c. Hu, F.-t. Bao, Z. Wang, and Q. Cai, “Numerical simulation of jet flow field and noise in nozzle,” Journal of Solid Rocket Technology, vol. 34, no. 4, pp. 436–439, 2011. View at Google Scholar
  9. S.-c. Hu, F.-t. Bao, and Y. Zhao, “Numerical simulation for multi-jet aeroacoustics,” Journal of Propulsion Technology, vol. 33, no. 3, pp. 430–435, 2012. View at Google Scholar
  10. X.-f. Xie, Z.-b. Ren, and X.-y. Cao, “Model building and analysis on infrared radiation characteristics of exhaust plume of cruise missils,” Opto-Electronic Engineering, vol. 36, no. 4, pp. 70–74, 2009. View at Google Scholar
  11. H.-h. Cai, N. Wan-sheng, and Z. Gang, “Impact of the inner nozzle surface on plume characteristics of LOX/kerosene engine,” Missile and Space Vehicles, vol. 5, pp. 35–38, 2015. View at Google Scholar
  12. S.-j. Feng, N. Wan-sheng, and X. Qing-fen, “Influence of combustion model in chamber on exhaust plume flow field and radiance,” Journal of Rocket Propulsion, vol. 32, no. 2, pp. 6–10, 2006. View at Google Scholar
  13. T. S. Wang, R. C. Farmer, and R. B. Edelman, “Turbulent combustion kinetics for complex hydrocarbon fuels,” in AIAA 26th Aerospace Sciences Meeting, Reno, USA, January 1988.
  14. R. B. Edelman and P. T. Harsha, “Laminar and turbulent gas dynamics in combustors current status,” in 34th Fluid Mechanics & Heat Transfer, Cleveland, OH, USA, March 1977.
  15. B. T. Vu, N. Bachchan, O. Peroomian, and V. Akdag, “Multiphase modeling of water injection on flame deflector,” in 21st AIAA Computational Fluid Dynamics Conference, San Diego, CA, USA, June 2013.
  16. C. Hong-hua, N. Wan-sheng, and H. Zhi-yong, “Impact effect of liquid rocket motor exhaust plume on launching platform,” Journal of Aerospace Power, vol. 31, no. 8, pp. 1995–2001, 2016. View at Google Scholar
  17. P. Pascal, F. Thomas, and V. Hilda, “Lox/methane and Lox/kerosene high thrust engine trade-off,” in 37th AIAA/ASME/SAE/ASEE Joint Propulsion, Salt Lake City, UT, USA, July 2001.