Volume 42 Issue 12
Dec.  2017
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LI Xin, LI Jiawen, WANG Jue, et al. Cavitation performance of inducer with helical static blades[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(12): 2654-2661. doi: 10.13700/j.bh.1001-5965.2015.0818(in Chinese)
Citation: LI Xin, LI Jiawen, WANG Jue, et al. Cavitation performance of inducer with helical static blades[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(12): 2654-2661. doi: 10.13700/j.bh.1001-5965.2015.0818(in Chinese)

Cavitation performance of inducer with helical static blades

doi: 10.13700/j.bh.1001-5965.2015.0818
Funds:  Science and Technology on Scramjet Laboratory
More Information
  • Corresponding author: LI Jiawen, Tel.:010-82338529, E-mail:lijiawen@buaa.edu.cn
  • Received Date: 17 Dec 2015
  • Accepted Date: 25 Mar 2016
  • Publish Date: 20 Dec 2017
  • In order to study internal flow pattern, the 3D flow in inducer with helical static blades is numerically computed by using the computational fluid dynamics (CFD). The suction and cavitation performance of the inducer are analyzed. The results show that the head increases with helical static blades, while the efficiency decreases resulted from the strong backflow in helical static blade channels. As the inlet pressure decreases, the cavitation develops along the radial direction, which is influenced by the centrifugal force. The choked helical static blade channels delay the appearance time of blocked inducer, so the cavitation performance of the inducer with helical static blades is improved.

     

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