Volume 24 Issue 1
Jan.  2009
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TANG Chan, CHANG Hai-ping. Numerical simulation of effusion holes on the longitudinal ripple heat shield[J]. Journal of Aerospace Power, 2009, 24(1): 18-24.
Citation: TANG Chan, CHANG Hai-ping. Numerical simulation of effusion holes on the longitudinal ripple heat shield[J]. Journal of Aerospace Power, 2009, 24(1): 18-24.

Numerical simulation of effusion holes on the longitudinal ripple heat shield

  • Received Date: 2007-11-21
  • Rev Recd Date: 2008-05-19
  • Publish Date: 2009-01-28
  • The numerical simulation was used to study the effusion holes on the longitudinal wavy liner in the combustor.The investigation focused on the parameters affecting cooling effectiveness,including: opening ratio,height of ripple board,diameter of holes and height of cooling passage.Given the same total flow effusion from holes,the results show that the heat shield gets a higher average cooling effectiveness when the opening ratio is 3% compared with 6%;cooling effectiveness is sensitive to the height of ripple board,the heat shield gets the highest cooling effectiveness when the dimensionless height of ripple board is 1% compared with 2% and 3.33%;but there is a little influence on the cooling effectiveness of the liner with the change of the diameter of holes and the height of cooling passage.

     

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