Spray and Combustion Characteristics of a Dump-type Ramjet Combustor

  • Lee, Choong-Won (Department of Mechanical Engineering, Kyungpook National University) ;
  • Moon, Su-Yeon (Department of Mechanical Engineering, Kyungpook National University) ;
  • Sohn, Chang-Hyun (Department of Mechanical Engineering, Kyungpook National University) ;
  • Youn, Hyun-Jin (Graduate School, Department of Mechanical Engineering, Kyungpook National University)
  • Published : 2003.12.01

Abstract

Spray and combustion characteristics of a dump-type ram-combustor equipped with a V-gutter flame holder were experimentally investigated. Spray penetrations with a change in airstream velocity, air stream temperature, and dynamic pressure ratio were measured to clarify the spray characteristics of a liquid jet injected into the subsonic vitiated airstream, which maintains a highly uniform velocity and temperature. An empirical equation was modified from Inamura's equation to compensate for experimental conditions. In the case of insufficient penetration, the flame in the ram-combustor was unstable, and vice versus in the case of sufficient penetration. When the flame holder was not equipped, the temperature at the center of the ram-combustor had a tendency to decrease due to the low penetration and insufficient mixing. Therefore, the temperature distribution was slanted to the low wall of the ram-combustor. These trends gradually disappeared as the length of the combustor became longer and the flame holder was equipped. Combustion efficiency increased when the length of the combustor was long and the flame holder was equipped. Especially, the effect of the flame holder was more dominant than that of the combustor length in light of combustion efficiency.

Keywords

References

  1. AGARD (Advisory Group for Aerospace research & Development) Advisory Report 323, 1994, pp.51
  2. Bayvel L. and Orzechowski, Z., 1993, 'Liquid Atomization,' pp. 168
  3. Inamura, T., Nagai, N., Hirai, T. and Asano, H., 1991, 'Disintegration Phenomena of Metalized Slurry Fuel Jets in High Speed Air Stream,' Proc. 5th International Conference on Liquid Atomization and Spray System (ICLASS-91), pp.839-846
  4. Inamura, T., Nagai, N., Yoshimura, K., Kumakawa, A. and Yatsuyanagi, N., 1995, 'Spray Formation and Spray Combustion in Ramjet Combustor,' Proc. The ASME/JSME Thermal Engineering, Honolulu, pp. 157-162
  5. Inamura, T. and Nagai, N., 1997, 'Spray Characteristics of Liquid Jet Traversing Subsonic Airstream,' Journal of Propulsion and Power, Vol. 13, No.1
  6. Kashiwagi, T., 1991, 'Study on afterburner of aircraft engine,' Ishikawajima- Harima Engineering Review (in Japan), Vol. 31, No.2, pp. 109-114
  7. Mattingly, Jack D., 1987, 'Aircraft Engine Design,' AIAA Education Series, pp. 324- 327
  8. Nejad, A. S. and Schetz, J. A., 1983 'Effects of Properties and Location in the Plume on Droplet Diameter for Injection in a Supersonic Stream,' AIAA Journal, Vol. 21, No.7, pp.956-961 https://doi.org/10.2514/3.8183
  9. Oates, G. C., 1978, 'The Aerothermodynamics of Aircraft Gas Turbine Engine,' AFAPL-TR78-52, July
  10. Shetz, J. A. and Padhye, A., 1977, 'Penetration and Breakup of Liquids in Subsonic Airstream,' AIAA Journal, Vol. 15, No. 10, pp. 1385-1390 https://doi.org/10.2514/3.60805
  11. Sjoblom, B., 1989, 'Full-Scale Liquid Fuel Ramjet Combustor Tests,' ISABE, No. 89-7027, pp.273-281
  12. Vinogradov, V. A., Kobigsky, S. A. and Petrov, M. D., 1995, 'Experimental Investigation of Kerosene Fuel Combustion in Supersonic Flow,' Journal of Propulsion and Power, Vol. 11, No.1, pp. 130-134 https://doi.org/10.2514/3.23850
  13. Waltrup, P. J., 1987, 'Liquid-Fueled Supersonic Combustion Ramjets; A Research Perspective,' Journal of Propulsion and Power, Vol. 3, pp.515-524 https://doi.org/10.2514/3.23019