Volume 39 Issue 12
Dec.  2024
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GAO Yaping, LIU Cunxi, ZHENG Zhaozhuo, et al. Study on the effect of swirl intensity for atomization characteristics in two-stage swirl combustor[J]. Journal of Aerospace Power, 2024, 39(12):20220312 doi: 10.13224/j.cnki.jasp.20220312
Citation: GAO Yaping, LIU Cunxi, ZHENG Zhaozhuo, et al. Study on the effect of swirl intensity for atomization characteristics in two-stage swirl combustor[J]. Journal of Aerospace Power, 2024, 39(12):20220312 doi: 10.13224/j.cnki.jasp.20220312

Study on the effect of swirl intensity for atomization characteristics in two-stage swirl combustor

doi: 10.13224/j.cnki.jasp.20220312
  • Received Date: 2022-05-06
    Available Online: 2024-08-14
  • Based on particle image velocimetry (PIV), plane laser scattering (PLS) and high speed granulometer, the atomization characteristics of prefilming air-blast atomizer under different swirl intensities were studied. The variation laws of fuel spatial distribution, spray cone angle and fuel particle size with swirl intensity were summarized. It was found that with the increase of the Sni, the axial velocity of the airflow at the outlet of the swirler decreased. Meanwhile, the axial length and radial width of the spray cone increased first and then decreased, and the spray cone angle and droplet diameter also showed the same trend. The central recirculation zone occurred within the Sno range from 0.695 to 0.987, whose starting position was X=70 mm. When the Sni was weak, the spray cone angle increased with the increase of Sno, and the droplet diameter decreased first and then increased with the increase of Sno. When Sni was strong, spray cone angle and droplet diameter were positively correlated with Sno. The results showed that the evolution law of spray characteristics of prefilming air-blast atomizer under different swirl intensities was explained, which could provide a theoretical support for improving atomization performance of swirl combustor.

     

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