Volume 23 Issue 9
Sep.  2008
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HUANG Ai-xia, WANG Suo-fang. Numerical simulation of flow and heat transfer inside co-rotating disc cavity with de-swirled radial inflow[J]. Journal of Aerospace Power, 2008, 23(9): 1684-1688.
Citation: HUANG Ai-xia, WANG Suo-fang. Numerical simulation of flow and heat transfer inside co-rotating disc cavity with de-swirled radial inflow[J]. Journal of Aerospace Power, 2008, 23(9): 1684-1688.

Numerical simulation of flow and heat transfer inside co-rotating disc cavity with de-swirled radial inflow

  • Received Date: 2007-09-06
  • Rev Recd Date: 2007-11-12
  • Publish Date: 2008-09-28
  • Numerical simulations were carried out to study the flow and heat transfer characteristics inside co-rotating disc cavity.The RNGturbulence model was applied to investigate the pressure loss across the disc cavity and the influences of non-dimensional mass flow coefficient,rotational Reynolds number and turbulent flow parameter on the flow and heat transfer.Results show that flow structure inside the cavity is mainly decided by turbulence flow parameter;under a constant value of rotational Reynolds number and the variation of flow rate,the pressure drop exhibits an "S-curve" behavior in which there are three different values of flow rate for each value of pressure drop;the pressure drop across the cavity can be effectively reduced with the use of de-swirled nozzles;the Nusselt number rises with the increase of non-dimensional mass flow coefficient and rotational Reynolds number.

     

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