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TURBINE-09. Proceedings of International Symposium on Heat Transfer in Gas Turbine Systems - 9−14 August 2009, Dedeman Hotel and Convention Center, Antalya, Turkey

DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst

Table of Contents:

TURBINE AIRFOIL LEADING EDGE STAGNATION AERODYNAMICS AND HEAT TRANSFER - A REVIEW
Lee S. Langston, Brian M. Holley
20 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.10
$25.00
RECENT PROGRESS IN NUMERICAL SIMULATION OF HIGHLY THREE-DIMENSIONAL TURBULENT FLOWS AND ENDWALL HEAT TRANSFER IN TURBINE BLADE CASCADES
Evgueni M. Smirnov
18 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.20
$25.00
EXPERIMENTAL INVESTIGATION OF TURNING FLOW EFFECTS ON INNOVATIVE TRAILING EDGE COOLING CONFIGURATIONS WITH ELLIPTIC PIN FINS
Carlo Carcasci, Francesco Simonetti
4 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.30
$25.00
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
8 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.40
$25.00
ADVANCED AERO-THERMAL INVESTIGATION OF HIGH PRESSURE TURBINE TIP FLOWS
Peter Vass, Tony Arts
12 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.50
$25.00
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
14 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.60
$25.00
AGUMENTED HEAT TRANSFER OF AN INTERNAL BLADE TIP BY FULL OR PARTIAL ARRAYS OF PIN-FINS
Gongnan Xie, Bengt Sunden, Lieke Wang, Esa Utriainien
13 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.70
$25.00
TURBINE AIRFOIL AEROTHERMAL CHARACTERISTICS IN FUTURE COAL-GAS BASED POWER GENERATION SYSTEMS
MinKing K. Chyu, Mary Anne Alvin
14 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.80
$25.00
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
11 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.90
$25.00
COUPLING STUDY BETWEEN HEAT TRANSFER AND AERODYNAMIC FLOW IN SQUARE-EDGED INLET
Phu Hung Nguyen, Viet Hung Nguyen, Eva Dorignac
12 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.100
$25.00
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
13 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.110
$25.00
CALCULATION OF GAS TURBINE BLADE TEMPERATURES USING AN ITERATIVE CONJUGATE HEAT TRANSFER APPROACH
Mangesh Kane, Savas Yavuzkurt
14 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.120
$25.00
EFFECT OF INTERNAL RIB CONFIGURATIONS ON THE DISCHARGE COEFFICIENT OF A 30-DEG INCLINED FILM COOLING HOLE
Christian Heneka, Achmed Schulz, Hans-Jorg Bauer
14 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.130
$25.00
INFLUENCE OF INTERNAL CYCLONE FLOW ON ADIABATIC FILM COOLING EFFECTIVENESS
Andreas Lerch, Heinz-Peter Schiffer
18 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.140
$25.00
STUDY ON THE THERMAL AND FLOW FIELDS OF SHAPED FILM COOLING HOLES
Kenichiro Takeishi, Tsuyoshi Kitamura, Masaharu Komiyama, Yutaka Oda, Shohei Mori
15 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.150
$25.00
FILM COOLING: BREAKING THE LIMITS OF DIFFUSION SHAPED HOLES
Ronald S. Bunker
22 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.160
$25.00
EXPERIMENTAL DETERMINATION OF THE AERO-THERMAL PERFORMANCE OF HIGH PRESSURE GAS TURBINE BLADES
Tony Arts
2 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.170
$25.00
EXPERIMENTAL STUDY OF EQUIVALENCE RATIO INFLUENCE ON THERMO-ACOUSTIC INSTABILITY IN GAS TURBINES
Nasser Seraj Mehdizadeh, Nozar Akbari, Reza Ebrahimi
8 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.180
$25.00
ANALYTICAL AND EXPERIMENTAL ANALYSIS OF REACTANTS VELOCITY EFFECT ON INSTABILITY OF PREMIXED COMBUSTION CHAMBER
Nasser Seraj Mehdizadeh, Nozar Akbari, Reza Ebrahimi
9 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.190
$25.00
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
16 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.200
$25.00
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
14 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.210
$25.00
FIRST MOMENT CLOSURE MODELING OF FILM COOLING EFFECTIVENESS IN SINGLE ROW OF CYLINDRICAL HOLES
Farzad Bazdidi-Tehrani, Hosein Foroutan, Mehran Rajabi-Zargarabadi
15 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.220
$25.00
FRONT BULKHEAD UPSTREAM EFFECT ON INLET IGV COMPRESSOR FLOW OF MS5002B GAS TURBINE
Rabah Dizene, Djamel Chekerker
12 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.230
$25.00
MODELING OF HEAT TRANSFER IN EXHAUST NOZZLE OF GAS TURBINES
Ozge Altun, Y. Erhan Boke
9 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.240
$25.00
A NEW UNSTEADY FLUID NETWORK APPROACH TO SIMULATE THE CHARACTERISTICS OF THE AIR SYSTEM OF A GAS TURBINE SYSTEM
Shengping Hou
12 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.250
$25.00
OPTIMIZATION OF A TURBINE VANE ENDWALL USING A COMBINED NATURAL AND NUMERICAL APPROACH
S. O. Neumann, H. Steinbruck, S. Zehner, Bernhard Weigand
1 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.260
$25.00
EFFECTS OF STATOR/ROTOR LEAKAGE FLOW AND AXISYMMETRIC CONTOURING ON ENDWALL ADIABATIC EFFECTIVENESS AND AERODYNAMIC LOSS
Ryan Erickson, Terrence W. Simon
18 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.270
$25.00
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
17 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.280
$25.00
IMPACT OF THE GEOMETRY ON THE IMPROVEMENT OF THE THERMAL TRANSFER OF THE TURBULENT FLOWS
Zineddine Ahmed Dellil, Abbes Azzi
11 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.290
$25.00
COMBINED HEAT EXCHANGE INTENSIFICATION TECHNIQUES AS A KEY TO DEVELOPMENT OF COMPACT HEAT EXCHANGERS FOR POWER GAS TURBINE UNITS
A. V. Sudarev
13 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.300
$25.00
PIV MEASUREMENTS OF THE FLOW IN A ROTATING CAVITY WITH A RADIAL INFLOW
Xiao Yu, Xiang Luo , Guoqiang Xu, Jining Sun
12 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.310
$25.00
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
12 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.320
$25.00
COMPARISON OF FILM COOLING IN THE PRESENCE OF VARIOUS MAINSTREAM PRESSURE GRADIENTS
Cun-liang Liu, Hui-ren Zhu, Guang-Chao Li, Du-chun Xu
18 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.330
$25.00
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
10 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.340
$25.00
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
16 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.350
$25.00
FILM COOLING SIMULATION AND CONTROL
Sumanta Acharya
22 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.360
$25.00
TURBINE VANE CASCADE HEAT TRANSFER PREDICTIONS USING A MODIFIED VERSION OF THE γ − Reοt % LAMINAR-TURBULENT TRANSITION MODEL
Evgueni M. Smirnov, Alexander Smirnovsky
11 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.370
$25.00
LARGE EDDY SIMULATION OF NON-ISOTHERMAL FLOW IN ROTOR/STATOR CAVITY
Ewa Tuliszka-Sznitko, Artur Zielinski, Wojciech Majchrowski
14 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.380
$25.00
COMPARISON OF COUNTER – ROTATING AND TRADITIONAL AXIAL AIRCRAFT LOW-PRESSURE TURBINES INTEGRAL AND DETAILED PERFORMACNES
Leonid Moroz, Petr Pagur, Yuri Govorushchenko, Kirill Grebennik
12 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.390
$25.00
NUMERICAL SIMULATION OF THE ENDWALL HEAT TRANSFER IN THE LANGSTON CASCADE
Alexander M. Levchenya, Evgueni M. Smirnov, Dmitry K. Zaytsev
8 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.400
$25.00
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
18 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.410
$25.00
HEAT TRANSFER AND FLOW TESTING IN ENGINE HP TURBINE COOLING SYSTEM DEVELOPMENT
Peter T. Ireland, Vikram Mittal, Howoong Namgoon, Dougal Jackson
16 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.420
$25.00
PREDICTING THE COOLANT FLOW AND HEAT TRANSFER IN RADIAL TURBINE BLADES
Aidin Panahi, Mozaffar Ali Mehrabian
20 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.430
$25.00
EFFECT OF ROTATION ON THE CYCLONE COOLING METHOD MASS TRANSFER MEASUREMENTS
Nils Winter, Heinz-Peter Schiffer
17 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.440
$25.00
TURBINE AIRFOIL LEADING EDGE STAGNATION AERODYNAMICS AND HEAT TRANSFER - A REVIEW
Lee S. Langston, Brian M. Holley
20 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.450
$25.00
RECENT STUDIES IN TURBINE BLADE INTERNAL COOLING
Je-Chin Han, Michael Huh
20 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.460
$25.00
MULTIPLE JET IMPINGEMENT − A REVIEW
Bernhard Weigand, Sebastian Spring
36 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.470
$25.00
INFLUENCE OF HEIGHT TO DIAMETER RATIO ON IMPINGEMENT HEAT TRANSFER ON EFFUSED CONCAVE SURFACE
M. Ashok Kumar, Bhamidi V. S. S. S. Prasad
16 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.480
$25.00
EXPERIMENTAL STUDY OF HEAT TRANSFER FROM IMPINGING JET WITH UPSTREAM AND DOWNSTREAM CROSSFLOW
Daniel Thibault, Matthieu Fenot, Gildas Lalizel, Eva Dorignac
10 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.490
$25.00
AN EXPERIMENTAL AND NUMERICAL INVESTIGATION OF IMPINGEMENT HEAT TRANSFER IN AIRFOILS LEADING-EDGE COOLING CHANNEL
Mohammad E. Taslim, A. Abdelrasoul
10 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.500
$25.00
LIQUID CRYSTAL THERMOGRAPHY FOR TRANSIENT HEAT TRANSFER MEASUREMENTS IN COMPLEX INTERNAL COOLING SYSTEMS
Rico Poser, Jens von Wolfersdorf
13 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.510
$25.00
EXPERIMENTAL AND THEORETICAL ANALYSIS OF HEAT TRANSFER CHARACTERISTICS IN A RECTANGULAR DUCT WITH JET IMPINGEMENT
Unal Uysal, F. Sahin, MinKing K. Chyu
12 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.520
$25.00
EXPERIMENTAL TURBINE AERO-HEAT TRANSFER STUDIES IN ROTATING RESEARCH FACILITIES
Cengiz Camci
21 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.530
$25.00
MIXING OF AIR AND CO2 STUDY ON A TURBINE BLADE
Yavuz Hakan Ozdemir, Seyfettin Bayraktar, Tamer Yilmaz
4 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.540
$25.00
Investigation of Film Cooled Rough Surfaces using Large Eddy Simulation
Prasad Kalghatgi, Sumanta Acharya
13 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.550
$25.00
THE EFFECT OF EMBEDDED VORTICES ON FILM COOLING WITH COMPOUND ANGLE ORIENTATIONS
Hyo Kyung Chung, Young Su Na, Joon Sik Lee
13 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.560
$25.00
A NOVEL METHOD FOR THE COMPUTATION OF CONJUGATE HEAT TRANSFER WITH COUPLED SOLVERS
Tom Verstraete, Rene Van den Braembussche
17 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.570
$25.00
APPLICATION OF ARTIFICIAL NEURAL NETWORK (ANN) METHOD TO EXERGETIC ANALYSES OF GAS TURBINES
Yilmaz Yoru, T. Hikmet Karakoc, Arif Hepbasli
15 pages
DOI: 10.1615/ICHMT.2009.HeatTransfGasTurbSyst.580
$25.00

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