Volume 22 Issue 11
Nov.  2007
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HAN Fei, LIU Yu. Heat transfer characteristics of axi-symmetrical nozzle and RS nozzle[J]. Journal of Aerospace Power, 2007, 22(11): 1947-1953.
Citation: HAN Fei, LIU Yu. Heat transfer characteristics of axi-symmetrical nozzle and RS nozzle[J]. Journal of Aerospace Power, 2007, 22(11): 1947-1953.

Heat transfer characteristics of axi-symmetrical nozzle and RS nozzle

  • Received Date: 2006-11-06
  • Rev Recd Date: 2007-04-10
  • Publish Date: 2007-11-28
  • To understand and compare different heat transfer characteristics of regenerative cooling in axi-symmetrical nozzle and round to square nozzle(RS nozzle),computational models of axi-symmetrical nozzle(thrust chamber) and RS nozzle(thrust chamber) were established.Numerical simulation was employed to investigate and compare fluid field,wall temperature,heat flux,coolant heat pick-up and pressure loss in the cooling circuit of axi-symmetrical nozzle and RS nozzle.The results show: In case of RS nozzle,because its contour is not continuous,peak values of wall temperature and heat flux exist at the location next to shape transformation,which leads to non-uniform temperature and heat flux distribution along the wall circumference.

     

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