Proceedings of International Symposium on Heat Transfer in Gas Turbine Systems
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Published By Begellhouse

9781567002638

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MIXING OF AIR AND CO2 STUDY ON A TURBINE BLADE

Proceedings of International Symposium on Heat Transfer in Gas Turbine Systems ◽

10.1615/ichmt.2009.heattransfgasturbsyst.540 ◽

2009 ◽

Author(s):

Yavuz Hakan Ozdemir ◽

Seyfettin Bayraktar ◽

Tamer Yilmaz

Keyword(s):

Turbine Blade

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EXPERIMENTAL TURBINE AERO-HEAT TRANSFER STUDIES IN ROTATING RESEARCH FACILITIES

Proceedings of International Symposium on Heat Transfer in Gas Turbine Systems ◽

10.1615/ichmt.2009.heattransfgasturbsyst.530 ◽

2009 ◽

Author(s):

Cengiz Camci

Keyword(s):

Heat Transfer ◽

Research Facilities

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MULTIPLE JET IMPINGEMENT - A REVIEW

Proceedings of International Symposium on Heat Transfer in Gas Turbine Systems ◽

10.1615/ichmt.2009.heattransfgasturbsyst.470 ◽

2009 ◽

Cited By ~ 10

Author(s):

Bernhard Weigand ◽

Sebastian Spring

Keyword(s):

Jet Impingement

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EFFECT OF ROTATION ON THE CYCLONE COOLING METHOD MASS TRANSFER MEASUREMENTS

Proceedings of International Symposium on Heat Transfer in Gas Turbine Systems ◽

10.1615/ichmt.2009.heattransfgasturbsyst.440 ◽

2009 ◽

Cited By ~ 2

Author(s):

Nils Winter ◽

Heinz-Peter Schiffer

Keyword(s):

Mass Transfer ◽

Cooling Method

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COMPARISON OF COUNTER ROTATING AND TRADITIONAL AXIAL AIRCRAFT LOW-PRESSURE TURBINES INTEGRAL AND DETAILED PERFORMACNES

Proceedings of International Symposium on Heat Transfer in Gas Turbine Systems ◽

10.1615/ichmt.2009.heattransfgasturbsyst.390 ◽

2009 ◽

Cited By ~ 1

Author(s):

Leonid Moroz ◽

Petr Pagur ◽

Yuri Govorushchenko ◽

Kirill Grebennik

Keyword(s):

Low Pressure

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EFFECT OF THE GEOMETRY OF FILM COOLING HOLES ON HEAT TRANSFER COEFFICIENT IN CONDITION OF VARIOUS MAINSTREAM PRESSURE GRADIENTS

Proceedings of International Symposium on Heat Transfer in Gas Turbine Systems ◽

10.1615/ichmt.2009.heattransfgasturbsyst.350 ◽

2009 ◽

Author(s):

Cun-liang Liu ◽

Xiao-wei Zhang ◽

Hui-ren Zhu ◽

Guang-Chao Li ◽

Du-chun Xu

Keyword(s):

Heat Transfer ◽

Heat Transfer Coefficient ◽

Transfer Coefficient ◽

Film Cooling ◽

Pressure Gradients ◽

Film Cooling Holes

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PIV MEASUREMENTS OF THE FLOW IN A ROTATING CAVITY WITH A RADIAL INFLOW

Proceedings of International Symposium on Heat Transfer in Gas Turbine Systems ◽

10.1615/ichmt.2009.heattransfgasturbsyst.310 ◽

2009 ◽

Author(s):

Xiao Yu ◽

X. Luo ◽

GuoQiang Xu ◽

J. N. Sun

Keyword(s):

Piv Measurements ◽

Rotating Cavity

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A NEW UNSTEADY FLUID NETWORK APPROACH TO SIMULATE THE CHARACTERISTICS OF THE AIR SYSTEM OF A GAS TURBINE SYSTEM

Proceedings of International Symposium on Heat Transfer in Gas Turbine Systems ◽

10.1615/ichmt.2009.heattransfgasturbsyst.250 ◽

2009 ◽

Author(s):

Shengping Hou

Keyword(s):

Gas Turbine ◽

Network Approach ◽

Fluid Network ◽

Air System ◽

Unsteady Fluid

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ANALYTICAL AND EXPERIMENTAL ANALYSIS OF REACTANTS VELOCITY EFFECT ON INSTABILITY OF PREMIXED COMBUSTION CHAMBER

Proceedings of International Symposium on Heat Transfer in Gas Turbine Systems ◽

10.1615/ichmt.2009.heattransfgasturbsyst.190 ◽

2009 ◽

Author(s):

Nasser Seraj Mehdizadeh ◽

Nozar Akbari ◽

Reza Ebrahimi

Keyword(s):

Combustion Chamber ◽

Experimental Analysis ◽

Premixed Combustion ◽

Velocity Effect

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EFFECT OF INTERNAL RIB CONFIGURATIONS ON THE DISCHARGE COEFFICIENT OF A 30-DEG INCLINED FILM COOLING HOLE

Proceedings of International Symposium on Heat Transfer in Gas Turbine Systems ◽

10.1615/ichmt.2009.heattransfgasturbsyst.130 ◽

2009 ◽

Author(s):

Christian Heneka ◽

Achmed Schulz ◽

Hans-Jorg Bauer

Keyword(s):

Film Cooling ◽

Discharge Coefficient ◽

Cooling Hole

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Proceedings of International Symposium on Heat Transfer in Gas Turbine SystemsLatest Publications

TOTAL DOCUMENTS

H-INDEX

Published By Begellhouse

MIXING OF AIR AND CO2 STUDY ON A TURBINE BLADE

EXPERIMENTAL TURBINE AERO-HEAT TRANSFER STUDIES IN ROTATING RESEARCH FACILITIES

MULTIPLE JET IMPINGEMENT - A REVIEW

EFFECT OF ROTATION ON THE CYCLONE COOLING METHOD MASS TRANSFER MEASUREMENTS

COMPARISON OF COUNTER  ROTATING AND TRADITIONAL AXIAL AIRCRAFT LOW-PRESSURE TURBINES INTEGRAL AND DETAILED PERFORMACNES

EFFECT OF THE GEOMETRY OF FILM COOLING HOLES ON HEAT TRANSFER COEFFICIENT IN CONDITION OF VARIOUS MAINSTREAM PRESSURE GRADIENTS

PIV MEASUREMENTS OF THE FLOW IN A ROTATING CAVITY WITH A RADIAL INFLOW

A NEW UNSTEADY FLUID NETWORK APPROACH TO SIMULATE THE CHARACTERISTICS OF THE AIR SYSTEM OF A GAS TURBINE SYSTEM

ANALYTICAL AND EXPERIMENTAL ANALYSIS OF REACTANTS VELOCITY EFFECT ON INSTABILITY OF PREMIXED COMBUSTION CHAMBER

EFFECT OF INTERNAL RIB CONFIGURATIONS ON THE DISCHARGE COEFFICIENT OF A 30-DEG INCLINED FILM COOLING HOLE

Proceedings of International Symposium on Heat Transfer in Gas Turbine Systems
Latest Publications

COMPARISON OF COUNTER ROTATING AND TRADITIONAL AXIAL AIRCRAFT LOW-PRESSURE TURBINES INTEGRAL AND DETAILED PERFORMACNES