Volume 43 Issue 1
Jan.  2017
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AN Honghui, NIE Wansheng. Influence of opening ratio on acoustic damping of orifice injector[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(1): 107-112. doi: 10.13700/j.bh.1001-5965.2016.0039(in Chinese)
Citation: AN Honghui, NIE Wansheng. Influence of opening ratio on acoustic damping of orifice injector[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(1): 107-112. doi: 10.13700/j.bh.1001-5965.2016.0039(in Chinese)

Influence of opening ratio on acoustic damping of orifice injector

doi: 10.13700/j.bh.1001-5965.2016.0039
Funds:

National Natural Science Foundation of China 91441123

More Information
  • Corresponding author: E-mail:nws1969@126.com
  • Received Date: 11 Jan 2016
  • Accepted Date: 25 Mar 2016
  • Publish Date: 20 Jan 2017
  • According to the length and the inlet boundary conditions of injector, the gas-liquid coaxial injectors of liquid rocket engine are simplified into four categories:1/4 wavelength closed tube, 1/2 wavelength closed tube, 1/4 wavelength open tube and 1/2 wavelength open tube. Linear acoustics is adopted to analyze the influence of the inlet opening ratio on the acoustic damping capability of the injector in order to obtain the law of the acoustic influence of opening ratio. It is found that the inlet opening rate has a very different effect on the damping capability of the injector under the conditions of standard length and optimal length. The damping capability can be greatly improved if the inlet opening rate and the length of the injector are chosen reasonably. The research results can provide reference for the optimum design of the length and inlet jet of the injectors, and acoustic damping of the combustion chamber.

     

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