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TURBINE-09. Proceedings of International Symposium on Heat Transfer in Gas Turbine Systems
August, 9-14, 2009, Antalya, Turkey

DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst


ISBN Print: 978-1-56700-263-8


Table of Contents:

TURBINE AIRFOIL LEADING EDGE STAGNATION AERODYNAMICS AND HEAT TRANSFER - A REVIEW Lee S. Langston, Brian M. Holley
page 20
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.10
RECENT PROGRESS IN NUMERICAL SIMULATION OF HIGHLY THREE-DIMENSIONAL TURBULENT FLOWS AND ENDWALL HEAT TRANSFER IN TURBINE BLADE CASCADES Evgueni M. Smirnov
page 18
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.20
EXPERIMENTAL INVESTIGATION OF TURNING FLOW EFFECTS ON INNOVATIVE TRAILING EDGE COOLING CONFIGURATIONS WITH ELLIPTIC PIN FINS Carlo Carcasci, Francesco Simonetti
page 4
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.30
HEAT TRANSFER CHARACTERISTICS ON TIP AND INNER RIM SURFACES OF A BLADEWITH SQUEALER RIM Jun Su Park, Dong Hyun Lee, Woo Jin Lee, Hyung-Hee Cho, Dong-Ho Rhee, Shin-Hyung Kang
page 8
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.40
ADVANCED AERO-THERMAL INVESTIGATION OF HIGH PRESSURE TURBINE TIP FLOWS Peter Vass, Tony Arts
page 12
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.50
TRAILING EDGE FILM COOLING OF GAS TURBINE AIRFOILS – EFFECTS OF EJECTION LIP GEOMETRY ON FILM COOLING EFFECTIVENESS AND HEAT TRANSFER Tim Horbach, Achmed Schulz, Hans-Jorg Bauer
page 14
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.60
AGUMENTED HEAT TRANSFER OF AN INTERNAL BLADE TIP BY FULL OR PARTIAL ARRAYS OF PIN-FINS Gongnan Xie, Bengt Sunden, Lieke Wang, Esa Utriainen
page 13
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.70
TURBINE AIRFOIL AEROTHERMAL CHARACTERISTICS IN FUTURE COAL-GAS BASED POWER GENERATION SYSTEMS MinKing K. Chyu, Mary Anne Alvin
page 14
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.80
THERMAL-MECHANICAL LIFE PREDICTION IN AFTER SHELL SECTION OF GAS TURBINE COMBUSTION LINER Kyung Min KIM, Yun Heung Jeon, Namgeon Yun, Dong Hyun Lee, Hyung-Hee Cho
page 11
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.90
COUPLING STUDY BETWEEN HEAT TRANSFER AND AERODYNAMIC FLOW IN SQUARE-EDGED INLET Phu Hung Nguyen, Viet Hung Nguyen, Eva Dorignac
page 12
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.100
HEAT TRANSFER INVESTIGATION OF THE SUB- AND SUPERCRITICAL FUEL FLOW THROUGH A U-TURN TUBE C. B. Zhang , Zhi Tao, Guoqiang Xu, Hongwu Deng , Jining Sun
page 13
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.110
CALCULATION OF GAS TURBINE BLADE TEMPERATURES USING AN ITERATIVE CONJUGATE HEAT TRANSFER APPROACH Mangesh Kane, Savas Yavuzkurt
page 14
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.120
EFFECT OF INTERNAL RIB CONFIGURATIONS ON THE DISCHARGE COEFFICIENT OF A 30-DEG INCLINED FILM COOLING HOLE Christian Heneka, Achmed Schulz, Hans-Jorg Bauer
page 14
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.130
INFLUENCE OF INTERNAL CYCLONE FLOW ON ADIABATIC FILM COOLING EFFECTIVENESS Andreas Lerch, Heinz-Peter Schiffer
page 18
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.140
STUDY ON THE THERMAL AND FLOW FIELDS OF SHAPED FILM COOLING HOLES Kenichiro Takeishi, Tsuyoshi Kitamura, Masaharu Komiyama, Yutaka Oda, Shohei Mori
page 15
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.150
FILM COOLING: BREAKING THE LIMITS OF DIFFUSION SHAPED HOLES Ronald S. Bunker
page 22
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.160
EXPERIMENTAL DETERMINATION OF THE AERO-THERMAL PERFORMANCE OF HIGH PRESSURE GAS TURBINE BLADES Tony Arts
page 2
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.170
EXPERIMENTAL STUDY OF EQUIVALENCE RATIO INFLUENCE ON THERMO-ACOUSTIC INSTABILITY IN GAS TURBINES Nasser Seraj Mehdizadeh, Nozar Akbari, Reza Ebrahimi
page 8
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.180
ANALYTICAL AND EXPERIMENTAL ANALYSIS OF REACTANTS VELOCITY EFFECT ON INSTABILITY OF PREMIXED COMBUSTION CHAMBER Nasser Seraj Mehdizadeh, Nozar Akbari, Reza Ebrahimi
page 9
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.190
A COMPARATIVE STUDY OF THE FILM COOLING HOLE CONFIGURATION EFFECTS ON THE LEADING EDGE OF ASYMMETRICAL TURBINE BLADE Mustapha Benabed, Abbes Azzi, B. A. Jubran
page 16
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.200
COMPARISON STUDY OF CLOSURE MODELS FOR MODELLING A FLOW ON CURVED AND FLAT PLATES. FILM COOLING APPLIED TO GAS TURBINE BLADE Rabah Dizene, Amar Berkache
page 14
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.210
FIRST MOMENT CLOSURE MODELING OF FILM COOLING EFFECTIVENESS IN SINGLE ROW OF CYLINDRICAL HOLES Farzad Bazdidi-Tehrani, Hosein Foroutan, Mehran Rajabi Zargarabadi
page 15
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.220
FRONT BULKHEAD UPSTREAM EFFECT ON INLET IGV COMPRESSOR FLOW OF MS5002B GAS TURBINE Rabah Dizene, Djamel Chekerker
page 12
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.230
MODELING OF HEAT TRANSFER IN EXHAUST NOZZLE OF GAS TURBINES Ozge Altun, Yakup Erhan Böke
page 9
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.240
A NEW UNSTEADY FLUID NETWORK APPROACH TO SIMULATE THE CHARACTERISTICS OF THE AIR SYSTEM OF A GAS TURBINE SYSTEM Shengping Hou
page 12
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.250
OPTIMIZATION OF A TURBINE VANE ENDWALL USING A COMBINED NATURAL AND NUMERICAL APPROACH S. O. Neumann, H. Steinbruck, S. Zehner, Bernhard Weigand
page 1
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.260
EFFECTS OF STATOR/ROTOR LEAKAGE FLOW AND AXISYMMETRIC CONTOURING ON ENDWALL ADIABATIC EFFECTIVENESS AND AERODYNAMIC LOSS Ryan Erickson, Terrence W. Simon
page 18
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.270
EFFECT OF GAP GEOMETRY ON THE COOLING EFFECTIVENESS OF THE WHEELSPACE COOLANT INJECTION UPSTREAM OF A ROW OF ROTOR BLADES M. Papa, V. Srinivasan, Richard J. Goldstein, Fabio Gori
page 17
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.280
IMPACT OF THE GEOMETRY ON THE IMPROVEMENT OF THE THERMAL TRANSFER OF THE TURBULENT FLOWS Zineddine Ahmed Dellil, Abbes Azzi
page 11
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.290
COMBINED HEAT EXCHANGE INTENSIFICATION TECHNIQUES AS A KEY TO DEVELOPMENT OF COMPACT HEAT EXCHANGERS FOR POWER GAS TURBINE UNITS A. V. Sudarev
page 13
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.300
PIV MEASUREMENTS OF THE FLOW IN A ROTATING CAVITY WITH A RADIAL INFLOW Xiao Yu, Xiang Luo , Guoqiang Xu, Jining Sun
page 12
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.310
STUDY ON INFLUENCE OF INITIAL WALL TEMPERATURE DISTRIBUTION ON THE TRANSIENT MEASUREMENT RESULTS OF FILM COOLING Cun-liang Liu, Hui-ren Zhu, Jiang-tao Bai, Du-chun Xu
page 12
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.320
COMPARISON OF FILM COOLING IN THE PRESENCE OF VARIOUS MAINSTREAM PRESSURE GRADIENTS Cun-liang Liu, Hui-ren Zhu, Guang-Chao Li, Du-chun Xu
page 18
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.330
A CORRELATION-BASED METHODOLOGY TO PREDICT THE FLOWSTRUCTURE OF FLOWS EMANATING FROM CYLINDRICAL HOLES WITH APPLICATION TO FILM COOLING Tilman auf dem Kampe, Stefan Volker
page 10
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.340
EFFECT OF THE GEOMETRY OF FILM COOLING HOLES ON HEAT TRANSFER COEFFICIENT IN CONDITION OF VARIOUS MAINSTREAM PRESSURE GRADIENTS Cun-liang Liu, Xiao-wei Zhang , Hui-ren Zhu, Guang-Chao Li, Du-chun Xu
page 16
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.350
FILM COOLING SIMULATION AND CONTROL Sumanta Acharya
page 22
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.360
TURBINE VANE CASCADE HEAT TRANSFER PREDICTIONS USING A MODIFIED VERSION OF THE γ − Reοt % LAMINAR-TURBULENT TRANSITION MODEL Evgueni M. Smirnov, Alexander Smirnovsky
page 11
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.370
LARGE EDDY SIMULATION OF NON-ISOTHERMAL FLOW IN ROTOR/STATOR CAVITY Ewa Tuliszka-Sznitko, Artur Zielinski, Wojciech Majchrowski
page 14
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.380
COMPARISON OF COUNTER – ROTATING AND TRADITIONAL AXIAL AIRCRAFT LOW-PRESSURE TURBINES INTEGRAL AND DETAILED PERFORMACNES Leonid Moroz, Petr Pagur, Yuri Govorushchenko, Kirill Grebennik
page 12
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.390
NUMERICAL SIMULATION OF THE ENDWALL HEAT TRANSFER IN THE LANGSTON CASCADE Alexander M. Levchenya, Evgueni M. Smirnov, Dmitry K. Zaytsev
page 8
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.400
AN EXPERIMENTAL STUDY OF AIRFOIL AND ENDWALL HEAT TRANSFER IN A LINEAR TURBINE BLADE CASCADE − SECONDARY FLOW AND SURFACE ROUGHNESS EFFECTS Marco Lorenz, Achmed Schulz, Hans-Jorg Bauer
page 18
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.410
HEAT TRANSFER AND FLOW TESTING IN ENGINE HP TURBINE COOLING SYSTEM DEVELOPMENT Peter T. Ireland, Vikram Mittal, Howoong Namgoon, Dougal Jackson
page 16
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.420
PREDICTING THE COOLANT FLOW AND HEAT TRANSFER IN RADIAL TURBINE BLADES Aidin Panahi, Mozaffar Ali Mehrabian
page 20
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.430
EFFECT OF ROTATION ON THE CYCLONE COOLING METHOD MASS TRANSFER MEASUREMENTS Nils Winter, Heinz-Peter Schiffer
page 17
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.440
TURBINE AIRFOIL LEADING EDGE STAGNATION AERODYNAMICS AND HEAT TRANSFER - A REVIEW Lee S. Langston, Brian M. Holley
page 20
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.450
RECENT STUDIES IN TURBINE BLADE INTERNAL COOLING Je-Chin Han, Michael Huh
page 20
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.460
MULTIPLE JET IMPINGEMENT − A REVIEW Bernhard Weigand, Sebastian Spring
page 36
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.470
INFLUENCE OF HEIGHT TO DIAMETER RATIO ON IMPINGEMENT HEAT TRANSFER ON EFFUSED CONCAVE SURFACE M. Ashok Kumar, Bhamidi V. S. S. S. Prasad
page 16
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.480
EXPERIMENTAL STUDY OF HEAT TRANSFER FROM IMPINGING JET WITH UPSTREAM AND DOWNSTREAM CROSSFLOW Daniel Thibault, Matthieu Fenot, Gildas Lalizel, Eva Dorignac
page 10
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.490
AN EXPERIMENTAL AND NUMERICAL INVESTIGATION OF IMPINGEMENT HEAT TRANSFER IN AIRFOILS LEADING-EDGE COOLING CHANNEL Mohammad E. Taslim, A. Abdelrasoul
page 10
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.500
LIQUID CRYSTAL THERMOGRAPHY FOR TRANSIENT HEAT TRANSFER MEASUREMENTS IN COMPLEX INTERNAL COOLING SYSTEMS Rico Poser, Jens von Wolfersdorf
page 13
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.510
EXPERIMENTAL AND THEORETICAL ANALYSIS OF HEAT TRANSFER CHARACTERISTICS IN A RECTANGULAR DUCT WITH JET IMPINGEMENT Unal UYSAL, F. Sahin, MinKing K. Chyu
page 12
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.520
EXPERIMENTAL TURBINE AERO-HEAT TRANSFER STUDIES IN ROTATING RESEARCH FACILITIES Cengiz Camci
page 21
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.530
MIXING OF AIR AND CO2 STUDY ON A TURBINE BLADE Yavuz Hakan Ozdemir, Seyfettin Bayraktar, Tamer Yilmaz
page 4
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.540
Investigation of Film Cooled Rough Surfaces using Large Eddy Simulation Prasad Kalghatgi, Sumanta Acharya
page 13
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.550
THE EFFECT OF EMBEDDED VORTICES ON FILM COOLING WITH COMPOUND ANGLE ORIENTATIONS Hyo Kyung Chung, Young Su Na, Joon Sik Lee
page 13
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.560
A NOVEL METHOD FOR THE COMPUTATION OF CONJUGATE HEAT TRANSFER WITH COUPLED SOLVERS Tom Verstraete, Rene Van den Braembussche
page 17
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.570
APPLICATION OF ARTIFICIAL NEURAL NETWORK (ANN) METHOD TO EXERGETIC ANALYSES OF GAS TURBINES Yilmaz Yoru, T. Hikmet Karakoc, Arif Hepbasli
page 15
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.580
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