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Study on Breakup of Conical Liquid Sheet under Varying Flow Conditions 被引量:3

不同液压条件下锥形液膜破碎的实验研究(英文)
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摘要 An experimental study on the breakup of a conical liquid sheet from a pressure swirl atomizer was conducted by using a Particle Image Velocimetry (PIV) system. The variation of wavelength, wave speed and amplitude of wave versus liquid pressure was obtained. The results indicate that the cone half angle increases with liquid pressure. The stripped half wavelength liquid fragment seems to break into a series of drops immediately and no obvious contraction from liquid fragment to ligament is seen. The recorded images also show that both short and long wavelength waves exist simultaneously, and influence the breakup of the conical liquid sheet. The result of this study is useful for the purpose of developing and verifying the atomization model of spray produced by a pressure swirl atomizer. An experimental study on the breakup of a conical liquid sheet from a pressure swirl atomizer was conducted by using a Particle Image Velocimetry (PIV) system. The variation of wavelength, wave speed and amplitude of wave versus liquid pressure was obtained. The results indicate that the cone half angle increases with liquid pressure. The stripped half wavelength liquid fragment seems to break into a series of drops immediately and no obvious contraction from liquid fragment to ligament is seen. The recorded images also show that both short and long wavelength waves exist simultaneously, and influence the breakup of the conical liquid sheet. The result of this study is useful for the purpose of developing and verifying the atomization model of spray produced by a pressure swirl atomizer.
出处 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2003年第1期12-14,共3页 中国航空学报(英文版)
基金 Aeronautical Science Foundation of China (99C5 10 91)
关键词 breakup of conical liquid sheet pressure swirl atomizer disturbance wave PIV breakup of conical liquid sheet pressure swirl atomizer disturbance wave PIV
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参考文献6

  • 1Feikema D A. Liquid film characteristics inside a pressureswirl atomizer[R]. AIAA Paper 98-3692,1998.
  • 2Holtzclaw D, Sokman T, Jeng S M, et al. Investigation of flow in a simplex fuel nozzle[R]. AIAA Paper 97-2970,1997.
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