ICHMT Turbine 2000

International Symposium on Heat Transfer in Gas Turbine Systems
13-18 August 2000
Golden Dolphin Holiday Village
Çeşme, Turkey

SESSION PROGRAM

Keynote lectures are allocated about 30 minutes, including 10 minutes for discussion
Contributed (oral) presentations are allocated 20 minutes including about 5 minutes for discussion

There will be no session on Wednesday and Friday afternoons.

Sunday, 13 August 2000

15:00 - 19:00 REGISTRATION

             Lobby area, Golden Dolphin Holiday Village

Monday, 14 August 2000

8:00 REGISTRATION

8:15 OPENING REMARKS

        Opening: R. J. Goldstein
                      Symposium Chairman, University of Minnesota, USA

        Welcome: F. Arinc
                       Secretary General of ICHMT, METU, Ankara, Turkey

                       U. Akbulut
                       Vice President, Middle East Technical University

8:30             SESSION 1: VANE EXTERNAL HEAT TRANSFER

Session Chair:T.W.SIMON              Vice-Chair:T.YOSHIDA

Invited talks:

Secondary flows in axial turbines - A review
        L.S. Langston

Heat transfer near turbine nozzle endwall
        M.K. Chyu

        Oral presentations

A new computer modelling for variable nozzle on an advanced supercharging engine
        G. Descombes, R. Duan, J. Julien, J-F. Pichouron

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

10:50 COFFEE BREAK

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

BREAK

15:30          SESSION 2: TRANSITION TO TURBULENCE AND ITS EFFECTS
                  ON HEAT TRANSFER AND DISC AND CAVITY HEAT TRANSFER

Session Chair:R.S.BUNKER              Vice-Chair:K.TAKEISHI

Invited talks:

Transition to turbulence under low-pressure turbine conditions
          T.W. Simon , R.W. Kaszeta

Some current research in rotating-disc systems
          J.M. Owen , M. Wilson

          Oral presentations

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

17:10 COFFEE BREAK

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

19:30 WELCOME RECEPTION-- GOLDEN DOLPHIN

Tuesday, 15 August 2000

8:30             SESSION 3: FILM COOLING -I

Session Chair:M.K.CHYU              Vice-Chair:A.I.LEONTIEV

Invited talks:

Unsteady flow modeling in turbine stage
          F. Martelli

The detailed structure and behaviour of discrete cooling jets in a turbine
          F. Leboeuf , O.Sgarzi

          Oral presentations:

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

10:50 COFFEE BREAK

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

12:30 POSTER SESSION

BREAK

15:30             SESSION 4: IMPINGEMENT COOLING / TIP HEAT TRANSFER

Session Chair:T.ARTS              Vice-Chair:J.C.HAN

Invited talks:

Impingement heat transfer in gas turbine systems
          B.Han, R.J. Goldstein

A review of turbine blade tip heat transfer
          R.S. Bunker

          Oral presentations

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

17:10 COFFEE BREAK

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

Wednesday, 16 August 2000

8:30             SESSION 5: COMBUSTOR COOLING TECHNOLOGY

Session Chair:D.K.HENNECKE              Vice-Chair:J.S.LEE

Invited talks:

Combustor liner technology in scope of reduced pollutant formation and rising thermal efficiencies
        A. Schulz

Cooling systems for ultra-high temperature turbines
        T. Yoshida

        Oral presentations:

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. Traverso, S. Duranti, 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

10:50 COFFEE BREAK

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

12:30 TRIP TO EPHESUS

Thursday, 17 August 2000

8:30             SESSION 6: FILM COOLING-II (mainly simulation)

Session Chair:L.S.LANGSTON              Vice-Chair:A.S.UCER

Invited talks:

Flow and heat transfer predictions for film cooling
        S. Acharya

Film cooling: What have we learnt from our measurements?
        T. Arts

        Oral presentations:

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

10:50 COFFEE BREAK

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

BREAK

15:30             SESSION 7: INTERNAL COOLING - I

Session Chair:F.LEBEOUF              Vice-Chair:M.KUMADA

Invited talks:

Recent developments in turbine blade internal cooling
          J-C. Han, S. Dutta

Heat transfer technology for internal passages of air-cooled blades for heavy-duty gas turbines
          B. Weigand , K. Semmler, J. von Wolfersdorf

          Oral presentations

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

17:10 COFFEE BREAK

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

PANEL DISCUSSION

Panelists : T. Arts, R.S. Bunker, R.J. Goldstein, D.K. Hennecke, K. Takeishi

20:30 CONFERENCE BANQUET, GOLDEN DOLPHIN

Friday, 18 August 2000

8:30             SESSION 8 - INTERNAL COOLING -II/ OPTIMIZATION OF TURBINE COOLING SYSTEMS

Session Chair:S. ACHARYA              Vice-Chair:J.M.OWEN

Invited talks:

Modelling and simulation of gas-turbine flow and heat transfer
        T.I-P. Shih

        Oral presentations

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

10:00 COFFEE BREAK

Secondary flow effect to heat transfer of a duct with discrete rib turbulators
          K. Tatsumi, H. Iwai, K. Inaoka, K. Suzuki

10:30 CLOSING REMARKS

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