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
相关论文
共 125 条
[91]  
PARK CW, 1997, ASME 42 INT GAS TURB, P1
[92]   WALL HEATING EFFECT ON LOCAL HEAT-TRANSFER IN A ROTATING 2-PASS SQUARE CHANNEL WITH 90-DEGREES RIB TURBULATORS [J].
PARSONS, JA ;
HAN, JC ;
ZHANG, YM .
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 1994, 37 (09) :1411-1420
[93]   EFFECT OF MODEL ORIENTATION AND WALL HEATING CONDITION ON LOCAL HEAT-TRANSFER IN A ROTATING 2-PASS SQUARE CHANNEL WITH RIB TURBULATORS [J].
PARSONS, JA ;
HAN, JC ;
ZHANG, YM .
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 1995, 38 (07) :1151-1159
[94]  
PRABHU SV, 1997, ASME 42 INT GAS TURB, P1
[95]   PREDICTION OF TURBULENT-FLOW AND HEAT-TRANSFER IN A RIBBED RECTANGULAR DUCT WITH AND WITHOUT ROTATION [J].
PRAKASH, C ;
ZERKLE, R .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1995, 117 (02) :255-264
[96]  
RAZGAITIS R, 1976, HEAT MASS TRANSFER P, V2, P831
[97]  
RIGBY DL, 2002, GT200230213 ASME
[98]  
RIGBY DL, 1998, ASME 43 INT GAS TURB, P1
[99]  
RIGBY DL, 1997, ASME 42 INT GAS TURB, P1
[100]  
Sampers W. F. J., 1992, ICHEME S SERIES, V2, P765