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SESSION 1: VANE EXTERNAL HEAT TRANSFER

• Keynote:Secondary flows in axial turbines - A review
  L.S. Langston
• Keynote:Heat transfer near turbine nozzle endwall
  M.K. Chyu
• A new computer modelling for variable nozzle on an advanced supercharging engine
  G. Descombes, J.F. Pichouron, J. Jullien, R. Duan
• Analysis of particle laden flow and heat transfer in turbine cascade and rocket nozzle
  H.H. Cho,W.S. Kim, M.S. Yu, J.C. Bae
• Convective heat transfer on an inlet guide vane
  M.L. Holmer, L.E. Eriksson, B. Sunden
• Effect of Reynolds number, turbulence level and periodic wake flow on heat transfer on low pressure turbine blades
  D. Suslov, A. Schulz, S. Wittig
• A conjugate heat transfer procedure for gas turbine blades
  G. Croce
• Contribution of heat transfer to turbine blades and vanes for high temperature industrial gas turbines
  K. Takeishi, S. Aoki
• Surface temperature mapping of gas turbine blading by means of high-resolution pyrometry
  S.L.F. Frank
• An improved transient method for the simultaneous determination of free-stream reference temperature and convective heat transfer coefficient : "the invariant h method"
  C. Camci
• Implementation of the "invariant h" method in liquid crystal thermometry based heat transfer research including film cooling
  C. Camci

SESSION 2: TRANSITION TO TURBULENCE AND ITS EFFECTS ON HEAT TRANSFER and DISC AND CAVITY HEAT TRANSFER

• Keynote:Transition to turbulence under low-pressure turbine conditions
  T.W. Simon, R.W. Kaszeta
• Keynote:Some current research in rotating-disc systems
  J.M. Owen, M. Wilson
• Studies on free stream turbulence as related to gas turbine heat transfer- a review of authors' past work and future implications
  S. Yavuzkurt, G.R. Iyer
• Modelling heat transfer in rotating disc cavities and application to the T56 engine
  J. Faragher, A. Ooi
• Verifying heat transfer analysis of high pressure cooled turbine blades and disk
  S. Yamawaki
• Computation of flow and heat transfer in rotating cavities with peripheral flow of cooling air
  M. Kilic
• The effect of labyrinth seal clearance on stator-well flow and windage heating
  H.K. Öztürk, A.B. Turner, P.R.N. Childs

SESSION 3: FILM COOLING -I

• Keynote:Unsteady flow modeling in turbine stage
  F. Martelli
• Keynote:The detailed structure and behaviour of discrete cooling jets in a turbine
  F. Leboeuf, O.Sgarzi
• Experimental investigation of film cooling flow induced by shaped holes on turbine blade
  S. Barthet, F. Bario
• Film cooling from rows of holes- effect of cooling hole shape and row arrangement on adiabatic effectiveness
  J. Dittmar, A. Schulz, S. Wittig, I.S. Jung, J.S. Lee
• Effects of bulk flow pulsations on film cooling with shaped holes
  H.W. Lee, J.S. Lee
• Film cooling: case of double rows of staggered jets
  P. Noiault, E. Foucault, J.L. Bousgarbies, E. Dorignac, J.J. Vullierme
• Characteristics of various film cooling jets injected in a conduit
  H. Takahashi, C. Nuntadusit, H. Kimoto, H. Ishida, T. Ukai, K. Takeishi
• Film cooling performance on curved walls with compound angle hole configuration
  P-H. Chen, M-S. Hung, P.P. Ding
• The variation of heat transfer coefficient, adiabatic effectiveness and aerodynamic loss with film cooling hole shape
  J. Sargison, S.M. Guo, M.L.G. Oldfield

POSTER SESSION

Characteristics of heat transfer on the high performance ceramic heat exchanger
K. Asato, M. Kumada, T. Yamamoto

SESSION 4: IMPINGEMENT COOLING / TIP HEAT TRANSFER

• Keynote:Impingement heat transfer in gas turbine systems
  B. Han, R.J. Goldstein
• Keynote:A review of turbine blade tip heat transfer
  R.S. Bunker
• Mach number effect on jet impingement heat transfer
  P. Brevet, E. Dorignac, J.J. Vullierme
• Numerical investigation of combined impingement and convection heat transfer
  A. Abdon, B. Sunden
• Heat/mass transfer characteristics on turbine shroud with blade tip clearance
  H.H. Cho, D.H. Rhee, J.H. Choi
• Heat transfer and flow characteristics on a gas turbine shroud
  M. Obata, M. Kumada, N. Ijichi

SESSION 5: COMBUSTOR COOLING TECHNOLOGY

• Keynote:Combustor liner technology in scope of reduced pollutant formation and rising thermal efficiencies
  A. Schulz
• Keynote:Cooling systems for ultra-high temperature turbines
  T. Yoshida
• Study of geometric effect on multihole cooling plates used for combustion chamber walls
  B. Leger, J.M. Emidio, F. Pardo
• Numerical simulation of three-dimensional reacting flow in gas turbine combustors. Part I: The NastComb solver
  S. Duranti, S. Traverso, F. Pittaluga
• Numerical simulation of three-dimensional reacting flow in gas turbine combustors. Part II: Detailed results
  S. Duranti, S. Traverso, F. Pittaluga
• Methane combustion and heat transfer in a turbo-gas combustor using a net of ideal reactors
  M. Belli, F.P. Di Maio, P. Fragiacomo
• Optimal control of swirl stabilized spray combustion using system identification approach
  S. Murugappan, S. Park, S. Acharya, A.M Annaswamy, E.J. Gutmark, A.F. Ghoniem

SESSION 6: FILM COOLING-II (mainly simulation)

• Keynote:Flow and heat transfer predictions for film cooling
  S. Acharya
• Keynote:Film cooling: What have we learnt from our measurements?
  T. Arts
• Numerical investigation of film cooling flow induced by cylindrical and shaped holes
  S. Barthet, P. Kulisa
• Numerical investigation of heat transfer on film-cooled turbine blades
  P. Ginibre, M. Lefebvre, N. Liamis
• A novel digital image processing system for the transient liquid crystal technique applied for heat transfer and film cooling measurements
  G. Vogel, A. Bölcs
• Comparison between two models of cooling surfaces using blowing
  L. Mathelin, F. Battaille, A. Lallemand
• Finite element analysis of flow field in the single hole film cooling technique
  F. Bazdidi-Tehrani, A.A. Mahmoodi
• Effects of entrance crossflow directions to film cooling holes
  C. Saumweber, A. Schulz, S. Wittig, M. Gritsch

SESSION 7: INTERNAL COOLING - I

• Keynote:Recent developments in turbine blade internal cooling
  J-C. Han, S. Dutta
• Keynote:Heat transfer technology for internal passages of air-cooled blades for heavy-duty gas turbines
  B. Weigand, K.Semmler, J.von Wolfersdorf
• Heat transfer in a dimpled two-pass channel
  S. Acharya, F. Zhou
• 3-D simulation of convection in asymmetrically heated turbine blade cooling channels
  I.Tari
• Detailed heat/mass transfer distributions in a rotating two-pass coolant channel with engine-near cross-section and smooth walls
  L. Rathjen, D.K. Hennecke, S. Bock, R. Kleinstück
• Analyses of heat transfer in stationary and rotating ribbed blade cooling passages using computational fluid dynamics
  R.A. Brewster, S. Jonnavithula
• Prediction of pressure loss and heat transfer in internal blade cooling passages
  K. Hermanson, S. Parneix, J. Von Wolfersdorf, K. Semmler
• Numerical simulation of local heat transfer in rotating two-pass square channels
  A.I. Kirillov, V.V. Ris, E.M. Simirnov, D.K. Zaitsev

SESSION 8: INTERNAL COOLING -II/ OPTIMIZATION OF TURBINE COOLING SYSTEMS

• Keynote:Modelling and simulation of gas-turbine flow and heat transfer
  T.I-P. Shih
• Experimental determination of average turbulent heat transfer and friction factor in stator internal rib- roughened cooling channels
  L. Battisti, P. Baggio
• Development of non-destructive inspection for the performance of thermal barrier coating
  M. Morinaga, T. Takahash
• Cycles of gas turbine engines with gas dynamic regeneration
  A.I. Leontiev
• Secondary flow effect to heat transfer of a duct with discrete rib turbulators
  K. Tatsumi, H. Iwai, K. Inaoka, K. Suzuki