Volume 36 Issue 9
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ZHOU Siyin, NIE Wansheng, BAO Heng. Mechanism of high frequency combustion instability control by pulsed discharge plasma in rocket engine[J]. Journal of Aerospace Power, 2021, 36(9): 1951-1961. doi: 10.13224/j.cnki.jasp.20210250
Citation: ZHOU Siyin, NIE Wansheng, BAO Heng. Mechanism of high frequency combustion instability control by pulsed discharge plasma in rocket engine[J]. Journal of Aerospace Power, 2021, 36(9): 1951-1961. doi: 10.13224/j.cnki.jasp.20210250
shu

Mechanism of high frequency combustion instability control by pulsed discharge plasma in rocket engine

doi: 10.13224/j.cnki.jasp.20210250

  • Department of Aerospace Science and Technology， Space Engineering University，Beijing 101416，China

  • Received Date: 2021-05-18
  • Publish Date: 2021-09-28
    Abstract
  • To explore the effect of plasma on high frequency combustion instability of rocket engine，a control scheme of pulsed quasi-direct current discharge plasmas was provided.The effects of pulsed discharge plasmas on average parameters and dynamic characteristics of combustor flow field were all numerically studied.Results showed that compared with the steady actuating way，the average temperature and pressure both decreased under the pulsed actuating way，yet the effect of plasma on the whole combustor can be ignored.Similar to that of steady actuating way，the plasma could depress the high frequency pressure oscillation within a certain time.However，the depression effect of pulsed discharge plasma was better than steady actuating way when suitable actuating parameters were adopted.According to the power spectral density plots，the characteristic dominant frequencies of combustor pressure oscillation were mainly determined by both the combustor intrinsic acoustic frequencies and the actuating frequencies for the pulsed actuating way.The power spectral density amplitude of dominant frequency decreased as the actuating frequency increased.The coupling charateristics of combustor pressure and heat release was not altered by the plasma.However，through decreasing the heat release rate，the pressure oscillating amplitude can be reduced，indicating that the pulsed discharge plasma can be used for depressing high frequency combustion instability.A pulsed actuating scheme with an actuating frequency of 50 kHz and a duty cycle of 20% can achieve the best control effect among the studied conditions.

     

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