首页> 外文会议>ASME turbo expo: turbine technical conference and exposition >AN EXPERIMENTAL INVESTIGATION OF IMPINGEMENT HEAT TRANSFER IN NARROW SPACE WITH FULL-HEIGHT PIN FINS
【24h】

AN EXPERIMENTAL INVESTIGATION OF IMPINGEMENT HEAT TRANSFER IN NARROW SPACE WITH FULL-HEIGHT PIN FINS

机译:全高销子在窄空间内冲击传热的实验研究

获取原文

摘要

An experimental study has been conducted on multiple-jet impingement heat transfer in a narrow space with full-height pin fins under maximum cross flow scheme. Transient liquid crystal thermography method has been used to obtain the detailed impingement heat transfer distribution for the Reynolds numbers from 15,000 to 30,000. The experimental study shows that the spanwisely-averaged Nusselt number ratio (Nu)/(Re~(0.8)Pr~(1/3)) is almost independent of Reynolds numbers, and the full-height pin-fin arrays can slightly improve the average Nusselt number on the endwall of the target plate by about 5.0%, and increase the pressure loss by up to about 17.9%. It is also found that heat transfer uniformity is also improved on the endwall of the target plate with pin fin arrays.
机译:在最大错流方案下,在具有全高销翅片的狭窄空间中,对多喷嘴撞击传热进行了实验研究。瞬态液晶热成像方法已用于获得雷诺数从15,000到30,000的详细的碰撞传热分布。实验研究表明,翼展平均Nusselt数比(Nu)/(Re〜(0.8)Pr〜(1/3))几乎与雷诺数无关,全高针翅阵列可以稍微改善雷诺数目标板上端壁上的平均Nusselt数增加了约5.0%,压力损失增加了约17.9%。还发现,在具有针翅阵列的目标板的端壁上,传热均匀性也得到了改善。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号