Volume 22 Issue 12
Dec.  2007
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SU Sheng, LIU Jian-jun, AN Bai-tao. Numerical simulation of conjugate heat transfer for an internally cooled 3-D turbine blade[J]. Journal of Aerospace Power, 2007, 22(12): 2018-2024.
Citation: SU Sheng, LIU Jian-jun, AN Bai-tao. Numerical simulation of conjugate heat transfer for an internally cooled 3-D turbine blade[J]. Journal of Aerospace Power, 2007, 22(12): 2018-2024.

Numerical simulation of conjugate heat transfer for an internally cooled 3-D turbine blade

  • Received Date: 2006-11-22
  • Rev Recd Date: 2007-04-03
  • Publish Date: 2007-12-28
  • To study the internal cooling technology of turbine blade,three types of blades,i.e.non-cooled blade using adiabatic boundary condition,non-cooled blade using conjugate heat transfer method,and air-cooled blade using conjugate heat transfer method,were studied.The results show that heat conductivity of the blade has a significant influence on blade temperature distribution;the structure of rib-roughened cooling and latticework cooling makes the blade temperature drop markedly.However,this leads to increased non-uniformity of blade temperature distribution and irregular heat transfer coefficient distribution on the blade surface.

     

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