Comparison of heat transfer augmentation techniques

被引:374
作者
Ligrani, PM [1 ]
Oliveira, MM
Blaskovich, T
机构
[1] Univ Utah, Salt Lake City, UT 84112 USA
[2] Pratt & Whitney Canada, United Technol Corp, Longueuil, PQ J4G 1A1, Canada
关键词
D O I
10.2514/2.1964
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A comparison of heat transfer augmentation techniques was presented. A variety of techniques were used for enhancing convective heat transfer rates in gas turbine engine passages used for internal cooling of turbine airfoils. These included rib turbulators, pin fins, dimpled surfaces, swirl chambers, and surface roughness. The overall objective of each device examined and future heat augmentation devices under development is improvement in high-thermal-performance parameters.
引用
收藏
页码:337 / 362
页数:26
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