Volume 42 Issue 8
Aug.  2016
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ZHANG Wenwei, KE Peng. Impact of channel curvature on microgravity membrane gas-liquid separation performance[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(8): 1639-1648. doi: 10.13700/j.bh.1001-5965.2015.0533(in Chinese)
Citation: ZHANG Wenwei, KE Peng. Impact of channel curvature on microgravity membrane gas-liquid separation performance[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(8): 1639-1648. doi: 10.13700/j.bh.1001-5965.2015.0533(in Chinese)

Impact of channel curvature on microgravity membrane gas-liquid separation performance

doi: 10.13700/j.bh.1001-5965.2015.0533
  • Received Date: 18 Aug 2015
  • Publish Date: 20 Aug 2016
  • The simulation research on the performance of microgravity membrane gas-liquid separation is of great significance for the design and optimization of gas-liquid separation technology. The Eulerian two-fluid model with an interface probability approximation method is introduced for the computability of multi-scale gas-liquid interface problem at inlet boundary in microgravity (inlet flow pattern problem), and the momentum source method is proposed for multi-scale geometric problem at membrane boundary. The model and the method provide a valid entry and permeable boundary for the simulation study. The influence of channel curvature on the membrane separation performance with typical operating parameters is studied, and the influence mechanism is analyzed in the view of flow morphologies and force contributions. The results show that the membrane separation performance reduces with channel curvature increasing, and the influence is related to inlet gas phase volume fraction; straight channel is suitable for membrane static gas-liquid separator.

     

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