HEAT-TRANSFER ANALYSIS ALONG BLADES OF A GAS-TURBINE STATOR BY THERMAL AND KINEMATIC BOUNDARY-LAYERS THEORY

被引：0

作者：

BECKO, Y ^{[1
]}

机构：

[1] WESTINGHOUSE ELECT CORP,RES LAB,CHARLEROI,BELGIUM

来源：

MECHANICAL ENGINEERING | 1975年 / 97卷 / 05期

关键词：

D O I：

暂无

中图分类号：

TH [机械、仪表工业];

学科分类号：

0802 ;

摘要：

引用

页码：54 / 54

页数：1

共 50 条

[1] MEASUREMENT OF HEAT-TRANSFER RATE TO A GAS-TURBINE STATOR
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[J]. JOURNAL OF ENGINEERING FOR POWER-TRANSACTIONS OF THE ASME, 1979, 101 (02): : 275 - 280
[2] CALCULATION OF HEAT-TRANSFER RATES TO GAS-TURBINE BLADES
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[J]. INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 1981, 24 (05) : 871 - 879
[3] HEAT-TRANSFER ANALYSIS IN BOUNDARY-LAYERS
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[4] BOUNDARY-LAYER THEORY CALCULATIONS OF HEAT-TRANSFER ON COOLED GAS-TURBINE BLADES AND COMPARISONS WITH MEASUREMENT VALUES
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[J]. ENERGIETECHNIK, 1979, 29 (12): : 469 - 474
[5] CALCULATION OF HEAT-TRANSFER TO CONVECTION-COOLED GAS-TURBINE BLADES
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[6] TURBULENT BOUNDARY-LAYERS WITH HEAT-TRANSFER
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[7] INTERACTING BOUNDARY-LAYERS AND HEAT-TRANSFER
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[8] HEAT-TRANSFER MEASUREMENT TECHNIQUES OF FILM-COOLING IN GAS-TURBINE BLADES
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[9] MODELING OF HEAT-TRANSFER PROCESSES IN BOUNDARY-LAYERS
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[10] FLOW TRANSITION PHENOMENA AND HEAT-TRANSFER OVER THE PRESSURE SURFACES OF GAS-TURBINE BLADES
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