As of Oct. 17, 2003

Time Room A Room B Room C Room D Room E Room F

Nov.3 MON 9:30 Opening Address 9:40 Keynote Speech 1 (at Main Hall) "Micro- or Small- Gas Turbines" Prof. Terry Simon University of Minnesota Chairperson: Dr. Kenichiro Takeishi (Mitsubishi Heavy Industries,Ltd.) 10:40 Break 10:50 Keynote Speech 2 (at Main Hall) "High Temperature Materials for Gas Turbine: The Present and Future" Dr. Hiroshi Harada National Institute of Materials Science Chairperson: Mr. Yomei Yoshioka (Toshiba Corporation) 11:50 Lunch 13:20 Superalloy 1 Unsteady Flow & Aero engine 1 Cascade Design Recuperator & Forum Noise 1 Heat Exchanger Wave Rotor 1 14:50 Break 15:10Forum 1産学協同 (at Main Hall) "Industry-University Cooperation in Gas Turbine Research" Co-chairs: Dr. David Wisler (General Electric), Prof. Toshinori Watanabe (University of Tokyo) 16:40 Break 17:00 Superalloy 2 Turbine Flow Aero engine 2 Combustion Blade Structure Forum Simulation Control Wave Rotor 2 19:00 Nov.4 TUE 9:00 Thermal Barrier Internal Flows 1 Heat Transfer & Micro Gas Throughflow Coating Flow Transition Turbine Modeling 11:00 Break 11:10 Keynote Speech 3 (at Main Hall) "Fuel Cell and Gas Turbine for Future Energy System" Dr. Takao Watanabe Central Research Institute of Electric Power Industry Chairperson: Mr. Katsuhide Hiraoka (National Maritime Research Institute) 12:10 Lunch 13:40 Keynote Speech 4 (at Main Hall) "Future View of Energy Supply and Role of Gas Turbine in Japan " Mr. Hiroyuki Ino Tokyo Electric Power Company Chairperson: Prof. Osamu Kawaguchi (Keio University) 14:30 Break 14:50 OS Internal Flows 2 Turbulence Model Combustor Advanced Diagnostics, Ultra Micro Gas Development Material Control & Turbine 1 Measurement 1

16:50 Break 17:00Forum 2各国のエネルギー政策 (at Main Hall) "Current Status and Strategy of Electricity and Energy Supply" Chairperson: Mr. Keizo Tsukagoshi (Mitsubishi Heavy Industries,Ltd.) 19:00 As of Oct. 17, 2003

Time Room A Room B Room C Room D Room E Room F

Nov.5 WED 9:00 OS Internal Flows 3 Ribbed Passage Low Emission Rotor Dynamics Diagnostics, Ultra Micro Gas Flow & Heat Combustor & Bearing Control & Turbine 2 Transfer Measurement 2

11:30 Break 11:40 Keynote Speech 5 (at Main Hall) "Combustion Technology for Current and Future Gas Turbines" Prof. Ann Dowling University of Cambridge Chairperson: Mr. Yasuhiro Kinoshita (Kawasaki Heavy Industries, Ltd) 12:40 Lunch 14:10 OS Development & Unsteady Flow & Conjugate Heat Performance Ultra Micro Gas Verification of Noise 2 Transfer Analysis Analysis of Gas Turbine 3 CFD codes Turbines: Intake Air Humidifying & Filtration 15:40 Break 15:50 Keynote Speech 6 (at Main Hall) "Recent Findings of Analytical Studies in Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines" Prof. Masanobu Namba Sojo University Chairperson: Prof. Toshinori Watanabe (The University of Tokyo) 16:50 17:00 Shuttle Bus Service to Banquet(Tower Hall Funabor 17:30 Tour of the Aquarium & Banquet(Tokyo Sea Life Park) Nov.6 THU 9:00 OS Surge/Stall 1 Industrial Gas Impingement & Combustor Performance Marine Gas Turbine & Power Film Cooling Design Analysis of Gas Turbines & Plant 1 Turbines & New Turbocharger Systems

11:00 Break 11:10 Keynote Speech Speech 7 7(at Main Hall) "Aeroengine Technology in 21st Century" Dr. Mike Benzakein GE Aircraft Engines Chairperson: Dr. Yoshiya Nakamura (Ishikawajima-Harima Heavy Industries Co.,Ltd.) 12:10 Lunch 13:30 Force/Vibration Surge/Stall 2 Industrial Gas Flows in Rotating Optimization & Performance Turbine & Power or Bended Duct Inverse Method Analytic Plant 2 Modellings & Tool

15:00 Break 15:20 Panel Discussion Discussion (at Main Hall) "Gas Turbines in the Future (Tentative)" Co-chairs: Prof. Nobuhide Kasagi (University of Tokyo) Mr. Kimio Sakata (Japan Aerospace Exploration Agency) 17:50 Closing Address 18:00 As of Oct. 17, 2003 Session Program November 3 Monday 13:20 - 14:50 Speaker's Name is underlined. Session A-1 Session B-1 Session C-1 Session D-1 Session E-1 Session F-1 Superalloy 1 Unsteady Flow & Noise 1 Aero engine 1 Cascade Design Recuperator & Heat Exchanger Forum: Wave Rotor 1

Chairpersons: Chairpersons: Chairpersons: Chairpersons: Chairpersons: Chairpersons: Dr. Ryohei Tanaka (Japan Ultra-high Temperature Prof. Satoru Yamamoto (Tohoku University) Dr. Arun K. Sehra (NASA, USA) Prof. Jian-jun LIU (Chinese Academy of Sciences, Mr. Yasuoki Tomita (Mitsubishi Heavy Prof. Toshio Nagashima (The University of Tokyo) Materials Reseach Institute) Dr. Yutaka Kawata (Mitsubishi Heavy Dr. Seishi Uchida (Mitsubishi Heavy Industries,Ltd.) P.R.China) Industries,Ltd.) Mr. Takashi Sakurai (Ishikawajima-Harima Heavy Industries,Ltd.) Dr. Atsumasa Yamamoto (Japan Aerospace Industries Co.,Ltd.) Exploration Agency)

13:20 TS-120 TS-047 TS-107 TS-041 TS-110 FR-301 Recovery of Material Properties in Service- Study on Noise Reduction in Turbofan (Effects on MG5 series Commercial Helicopter Engine Novel Blade-free Turbomachine Concept for Applications of Compact Size Recuperator on Preliminary Design Procedure for Gas Turbine Degraded Gas Turbine Blades Performance and Noise by Improving Outlet Angle Development and Utilization Microgasturbine Engine Applications (Part 1. Vehicle Microturbines Topping Reverse-Flow Wave Rotors of Impeller) Design.Design Characteristics. Metal Model Realization)

A. Ito (Chubu Electric Power Co.,Ltd.), Y. Kagiya, H. T. Hirano (Hosei University), G. Minorikawa, S. S. Uchida (Mitsubishi Heavy Industries, Ltd.), Y. A. Soudarev (Boyko Research-Engineering R. Cui (Shenyang Liming Aero-Engine Group P. Akbari (Michigan State University, USA),N. Watanabe, H. Takagi, D. Saito, Y. Yoshioka, H. Suzuki, S. Mizuki Nagashima, K. Shimauchi “Ceramic Heat Engines” Center (NIZ KTD), Corp., P.R.China), X. Wu, K. Wang, B. Deng Müller Ito, J. Ishii Russia), A. Souryaninov, V. Tikhoplav, A. Molchanov, P. Avran, L. Lelait

13:50 TS-123 TS-048 TS-104 TS-042 TS-067 FR-302 Development and Evaluation of High Strength Ni- Unsteady Three-Dimensional Navier-Stokes Overview on 4 Years Achievements of Research Development Status of a Fore-Loaded Turbine Development of CMC Heat Exchanger and Its Introductory Investigation of Micro Wave Rotor base Single Crystal Superalloy,TMS-82+ Simulations of Turbine Rotor-Stator Interaction and Technology Development of Environmentally Blade Thermo-fluid Dynamics Performance Using Multi-Airfoil Compatible Propulsion System for Next- Generation Supersonic Transport (ESPR project) T. Hino (Toshiba Corporation), Y. Yoshioka, Y. D. Biswas (Toshiba Corporation), T. Takamatsu, H. Y. Fujitsuna (Engineering Research Association for H. Taki (Kawasaki Heavy Industries, Ltd.), D. T. Yoshida (Japan Aerospace Exploration Agency), K. Okamoto (The University of Tokyo), T. Koizumi, T. Kobayashi H. Harada Iwasaki Supersonic Transport Propulsion System) Kataoka, H. Kato, K. Hashimoto T. Kumagai, T. Yamane Nagashima, K. Yamaguchi

14:20 TS-124 TS-049 TS-105 TS-043 TS-112 FR-303 Development of A Grain Defects Resistant Ni- Numerical and Experimental Investigation of the Technology Requirements for Revolutionary CFD Design of a 8:1 Pressure Ratio Centrifugal Development of Large Scale Recuperator for Gas Internal Combustion Wave Rotors for Gas Turbine Based Single Crystal Superalloy YH61 Unsteady Flow Field in a Transonic Centrifugal Propulsion Systems of the 21st Century Compressor Turbine Engine Enhancement Compressor H. Tamaki (Hitachi, Ltd.), A. Okayama, A. H. Krain (DLR, Germany), C. Hah W. Whitlow, Jr. (NASA Glenn Research Center, V. I. Mileshin (Central Institute of Aviation Motors, R. Akiyoshi （Ishikawajima-Harima Heavy Industries R. Nalim (Indiana University Purdue University Yoshinari , K. Kageyama , K. Sato, T. Ohno USA), J. M. Earls , V. W. Wessel Russia), A. N. Startsev, I. K. Orekhov Co.,ltd.）, K. Imai, T. Sioda, K. Ito, M. Hori Indianapolis (IUPUI), USA) , K. Pekkan

November 3 Monday 17:00 - 19:00 Session A-2 Session B-2 Session C-2 Session D-2 Session E-2 Forum 3 Superalloy 2 Turbine Flow Simulation Aero engine 2 Combustion Control Blade Structure Forum: Wave Rotor 2

Chairpersons: Chairpersons: Chairpersons: Chairpersons: Chairpersons: Chairpersons: Mr. Koji Take (Kawasaki Heavy Industries, Ltd) Prof. Hyung Hee Cho (Yonsei University, Korea) Dr. Jih-Fen Lei (NASA Glenn Research Center, Dr. Kazuo Suzuki (Japan Aerospace Exploration Dr. Stanislaw Strzelecki (Technical University of Prof. Toshio Nagashima (The University of Tokyo) USA) Agency) Lodz, Poland) Dr. Yoshiya Nakamura (Ishikawajima-Harima Mr. Yasuhiro Kinoshita (Kawasaki Heavy Industries, Prof. Sigehiko Kaneko (The University of Tokyo) Heavy Industries Co.,Ltd.) Ltd)

17:00 TS-121 TS-070 TS-106 TS-146 TS-009 FR-304 Oral Presentation Only Development of the Third Generation Single Turbulent Flow Computation in Film-Cooling Revolutionary Propulsion Systems for 21st Application of the Helmholtz Resonator for Bird Impact Analysis of Pre-Stressed Fan Blades The Wave Rotor for Gas Turbines: Description, Crystal Superalloy for Power Generation Gas Turbine Cascades Century Aviation Reducing the Combustion Oscillation in a Gas Using Explicit Finite Element Code Operation and Use Turbines Turbine A. Yoshinari (Hitachi Ltd.), R. Hashizume, Y. B. Kurmanov (ALSTOM Power Uniturbo, Russia), A. K. Sehra (NASA Glenn Research Center, USA), S. Yamanaka (Toshiba Corporation), F. Maeda, K. R. Jain (Gas Turbine Research Establishment, Y. Ribaud (ONERA, France) Murata, M. Morinaga M. Namba, G. Podvidz J. Shin Shioda, K. Iwabuchi, T. Tsuchiya, M. Okamoto India), K. Ramachandra

17:30 TS-118 TS-071 TS-108 TS-147 TS-010 FR-305 Oral Presentation Only Mechanical Properties and Castability of 4th Approach to a New Scheme Film Cooling Design and Test of Transonic Compressor Rotor Advanced Monitoring System For Combustor Reduction of Vibratory Stress of Compressor Autonomous Pressure Wave Compressor Devise Generation Ni-base Single Crystal Superalloy Enhancement by Jet Path Control and Reduction with Tandem Cascade Pressure Fluctuation Blade by Use of Asymmetric Vane Spacing TMS-138 Mixing zones Using Coupled Jets Y. Aoki (Ishikawajima-Harima Heavy Industries Co., A.Javadi (Sharif University of Technology, Iran), Y. Sakai (Kawasaki Heavy Industries, LTD), A. H.Iba (Mitsubishi Heavy Industries, LTD.), M. Y. Kaneko (Mitsubishi Heavy Industries, Ltd.), K. J. Piechna (Warsaw Technical University, Poland) Ltd.), M. Arai, K. Chikugo, Y. Koizumi, H. Harada K.Javadi, M. Taeibi-Rahni , M. Darbandi Matsuoka, S. Suga, K. Hashimoto Nomura, T. Kawakami, T. Koga Mori, H.Okui

18:00 TS-119 TS-072 TS-109 TS-148 TS-011 FR-306 Oral Presentation Only Development of a Next Generation Ni-base Single A Three-Dimensional Navier-Stokes Simulation of A Booster Stage with Tandem Cascade Rotor for Sound Emission from Laminar Diffusion Flame with Blade-Strength Assessment of a Marine The General Compatibility Conditions of the Crystal Superalloy A Film-Cooled Turbine Stage Fan Engine Controlled Oscillatory Fuel Flow Turbocharger under Development Nonstationary Compressible Flow in Stationary Periodic and Materially Balanced Pressure Wave Machine Y. Koizumi (National Institute for Materials Science T. Nishizawa (Japan Aerospace Exploration S. Suga (Kawasaki Heavy Industries, Ltd.), A. K. Harumi (National Maritime Research Institute), F. Iwaki (Ishikawajima-Harima Industries Co., Ltd.), H. A. Nour Eldin (University of Wuppertal, (NIMS)), T.Kobayashi, Z. Jianxin, T.Yokokawa, Agency), K. Saiki, O. Nozaki, K. Kikuchi Matsuoka , Y. Sakai, K. Hashimoto M. Ikame, T. Kishi, K. Hiraoka, H. Oka K. Mitsubori, H. Taguchi, M. Obata, A. R. Mech Germany) H.Harada, Y.Aoki, M.Arai 18:30 TS-122 TS-073 TS-132 TS-012 FR-307 Oral Presentation Only Development of a Gas Turbine Design Program Numerical Investigation of the Flow Field in HP LES of Combustion Instabilities in a Lean Premixed Interface Construction for Thermal Stress Analysis Wave Rotor - A Review of the Work of Power Jets Coupled with an Alloy Design Program - A Virtual Turbine Stage Gas Turbine Combustor in Virtual Turbine and Its Application Ltd. and Univ. of Calgary Turbine

H. Saeki (Toshiba Corporation), T. Yokokawa, H. F. Martelli (University of Florence, Italy), P. Adami, J. Shinjo (Japan Aerospace Exploration Agency), Y. J. Chen (Japan Aerospace Exploration Agency), A. J. A. C. Kentfield (University of Calgary, Canada) Harada, Y. Fukuyama, T. Yoshida E. Belardini Mizobuchi, S. Ogawa Ogawa, R. Hashimoto, T. Yoshida

1 As of Oct. 17, 2003 November 4 Tuesday 9:00 - 11:00 Speaker's Name is underlined. Session A-3 Session B-3 Session C-3 Session D-3 Session F-3 Thermal Barrier Coating Internal Flows 1 Heat Transfer & Flow Transition Micro Gas Turbine Throughflow Modeling

Chairpersons: Chairpersons: Chairpersons: Chairpersons: Chairpersons: Dr. Yoshiatsu Kojima (Hitachi Ltd.) Prof. Wolfgang Schröder (Aachen University, Prof. Lee Langston (University of Connecticut, Prof. Terry Simon (University of Minnesota, USA) Prof. Xiaofeng Sun (Beijing University of Mr. Hideaki Kaneko (Mitsubishi Heavy Industries, Germany) USA) Dr. Toshiaki Tsuchiya (Tokyo Electric Power Aeronautics and Astronautics, P.R.China) Ltd.) Prof. Makoto Yamamoto (Tokyo University of Mr. Nobuaki Kizuka (Hitachi Ltd.) Company) Science)

9:00 TS-129 TS-031 TS-066 TS-115 TS-050 Recent Developments in the Field of Plasma- The Simulation of 3D Flows in Blade Rows and Construction of Cooling Effectiveness Database The Development of 300kW Class High Efficiency Theory and Design of the Regenerative Flow Sprayed Thermal Barrier Coatings Exhaust Systems using a Multiblock Navier- Applied to the Virtual Gas Turbine in HTM21 Micro Gas Turbine “RGT3R” Compressor Strokes Solver Project R. Vaßen (Institut für Werkstoffe und Verfahren der J. Liu (Chinese Academy of Sciences, P.R.China) M. Matsushita (Japan Aerospace Exploration R. Shibata (Niigata Power Systems Co., Ltd.), Y. A. Engeda (Michigan State University, USA), M. Energietechnik (IWV 1), Germany), J. -E.. Döring, Agency), T. Yoshida Nakayama, S. Machiya, K. Kobayashi Raheel M. Dietrich, H. Lehmann, D. Stöver 9:30 TS-130 TS-032 TS-068 TS-116 TS-051 Development and Evaluation of Thermal Barrier 3D Configuration of Shock Wave in Transonic Effects of Periodic Wake Passing Upon Bypass Microturbocompressor Fuel Cell - Based Plants for Flow in a High Speed Compressor Due to Coatings for the 1700 ℃ -class Closed-Cycle Gas Centrifugal Impeller Using 2D-PIV Transition of Blade Boundary Layer and Unsteady Hybrid Engine Applications Axisymmetric Tip Clearance Turbine Corresponding to CO2 Collection Loss

M. Okada (Central Research Institute of Electric M. Hojo (Japan Aerospace Exploration Agency), H. E. Koyabu (Sophia University) , K. Funazaki, M. A. Soudarev (Boyko Research-Engineering H. S. Joo (Seoul National University, Korea), S. J. Power Industry), M. Nakayama, T. Torigoe, T. Hayami, S. Aramaki Kimura “Ceramic Heat Engines” Center (NIZ KTD), Song Kameda, H. Arikawa, T. Hisamatsu Russia), A. Souryaninov, A. Molchanov, P. Arvan, L. Lelait 10:00 TS-131 TS-033 TS-069 TS-117 TS-052 Thermal Conductivity and Sintering Behavior of Numerical Study on Blade Roughness Effect on Studies on Effects of Periodic Wake Passing upon Combined Thermal Efficiency Evaluation and The Reduced Order Through-Flow Modeling of Hafnia-based Thermal Barrier Coating Using EB- the Performance of Turbomachines a Blade Leading Edge Separation Bubble: Dynamic Characteristics of Micro Gas Turbine Axial Turbomachinery PVD Transitional Behaviors of Separated Boundary Centered Co-generation System Layer K. Matsumoto (Toshiba Corporation), Y. Itoh, Y. S. H. Kang (Seoul National University, Korea), Y. S. K. Funazaki (Iwate University), K. Yamada, Y. Kato S. Kaneko (The University of Tokyo ), G. O. Dubitsky (Concepts NREC, USA), A. Ishiwata Kang, K. H. Han Fukuyama, T. Watanabe Wiedermann, T. Nakano, J. Perera

TS-113 Development of a Small Jet Engine Test System for University Education

M. Tanabe (Nihon University), T. Kuwahara, K. Aoki

November 4 Tuesday 14:50 - 16:50 Organized Session 1 Session B-4 Session C-4 Session D-4 Session E-4 Session F-4 Ultra Micro Gas Turbine 1 Internal Flows 2 Turbulence Model Combustor Development Advanced Material Diagnostics, Control & Measurement 1

Chairpersons: Chairpersons: Chairpersons: Chairpersons: Chairpersons: Chairpersons: Prof. Yves Ribaud (ONERA, France) Prof. Abraham Engeda (Michigan State University, Dr. Robert Kiml (Tokyo University of A&T) Dr. George K. Vedeshkin (Central Institute of Dr. Hiroshi Harada (National Institute for Materials Mr. Masanori Endoh (Japan Aerospace Exploration Prof. Shimpei Mizuki (Housei University) USA) Dr. Yoshitaka Fukuyama (Japan Aerospace Aviation Motor, Russia) Science) Agency) Dr. Osamu Nozaki (Japan Aerospace Exploration Exploration Agency) Dr. Takashi Tamaru (Central Research Institute of Agency) Electric Power Industry)

14:50 OS-101 TS-027 TS-059 TS-149 TS-126 TS-001 Aerothermal Optimization of Micro-gasturbine Numerical Simulation of Stall Suppression by Micro The SST Turbulence Model with Improved Wall The Effects of Specifications of a Fuel Supply Unit Low Cost Manufacturing Process of Titanium Matrix Fault Diagnosis System for an Industrial Gas Compressor Including Heat Transfer Air Injection in a Low-Speed Axial Compressor Treatment for Heat Transfer Predictions in Gas with a New Concept for a Dry Low NOx Gas Composite Ring Turbine by Means of Neural Networks Turbines Turbine Combustor R. A. Van den Braembussche (von Karman G. Xu (Chinese Academy of Sciences, P.R.China), F. Menter (ANSYS CFX, Germany), J. Carregal T. Wakabayashi (OSAKA GAS CO., LTD.), K. A. Kono (Mitsubishi Heavy Industries, Ltd.), T. J. Arriagada (Lund University, Sweden), M. Genrup, Institute for Fluid Dynamics, Belgium), A. A. Işlek, H. Zhang, C. Nie, W. Huang, J. Chen Ferreira, T. Esch, B. Konno Moriya, S. Ito, S. Koga, K. Shimodaira, Y. Yamada, M. Hirota, Y. Kawachi A. Loberg, M. Assadi Z. Alsalihi Kurosawa, K. Suzuki, O. Kawaguchi 15:20 OS-102 TS-028 TS-060 TS-150 TS-127 TS-002 Conceptual Design of Recuperator for Ultramicro Numerical Investigation of two 3-D Designed Large-Eddy Simulation of Film Cooling The Development of LPP Combustor for ESPR Development of Turbine Disk Materials for Aircraft A Study on Intelligent Performance Diagnostics of Gas Turbine Profiles in a 2-stage Turbine with Shrouded Engines a Gas Turbine Engine Using Neural Networks Bladings T. Nagasaki (Tokyo Institute of Technology), R. D. E. Bohn (Aachen University, Germary), I. X. Guo (Aachen University, Germany), W. T. Oda (Kawasaki Heavy Industries, Ltd.), Y. S. Takahashi (Ishikawajima-Harima Heavy C. D. Kong (Chosun University, Korea), J. Y. Ki , M. Tokue, S. Kashima, Y. Ito Balkowski, C. Tümmers, M. Sell Schröder, M. Meinke Kinoshita, M. Kobayashi, H. Ninomiya, H. Kimura, Industries Co., Ltd.), S. Nishikiori, M. Hosoya, M. C. Kang, S. H. Kho S. Hayashi, H. Yamada, K. Shimodaira Arai, M. Takekawa, K. Tahara 15:50 OS-103 TS-029 TS-061 TS-151 TS-125 TS-003 Towards the Development of Finger-Top Gas Aerodynamic Blade Optimal Design of Second-moment Turbulence Closure in Prediction Development of Ultra Low-NOx Combustor Technology Research on High Efficiency Gas Neural Networks for the Study of Gas Turbine Turbines Turbomachinery of Channel Flow with System Rotation Technology for Next Generation Supersonic Turbines Utilizing Melt-Growth Composite Engines Air System Transport Engines in ESPR Project Ceramics E. Matsuo (The University of Tokyo,), H. Yoshiki, T. R. S. Amano (University of Wisconsin-Milwaukee, M. Ichikawa (Keio University), S. Obi, S. Masuda S. Hayashi (Japan Aerospace Exploration Agency), K. Kobayashi (Engineering Association for High G. Torella (Italian Airforce Academy, Italy), F. Nagashima, C. Kato USA), C. Xu H. Yamada, K. Shimodaira, S. Yoshida, T. Oda, H. Performance Gas Turbines(HPGT)), Y. Waku, N. Gamma , G. Palmesano Ninomiya, B. Jones Nakagawa, S. Yokoi TS-030 TS-062 TS-152 TS-128 TS-004 Numerical Analysis of Tip Leakage Flow Field in a Large-Eddy Simulation of Trailing-Edge Blowing Study on Pre-vaporized and Premixed Gas Research and Development of Niobium-Based Statistical Analyses to Improve Gas Turbine Transonic Axial Compressor Rotor Turbine Combustion Technology for High Carbon Superalloys for Hot Components of Gas Turbines Diagnostics Reliability Ratio Fuel (HCRF) K. Yamada (Iwate University), M. Furukawa, M. J. Krömer (Rheinisch-Westfälische Hochschule Y. Marutani (Ishikawajima-Harima Heavy Industries R. Tanaka (Japan Ultra-high Temperature R. Bettocchi (University of Ferrara, Italy), M. Pinelli, Inoue, K. Funazaki Aachen ,Germany), M. Meinke, W. Schröder Co, Ltd.), T. Fujimori, D. Riechelmann, T. Mizutani, Materials Research Institute(JUTEMI)), A. P. R. Spina, M. Venturini M. Mikami Kasama， M. Fujikura, I. Iwanaga, H. Tanaka, Y. Matsumura

2 As of Oct. 17, 2003 November 5 Wednesday 9:00 - 11:30 Speaker's Name is underlined. Organized Session 2 Session B-5 Session C-5 Session D-5 Session E-5 Session F-5 Ultra Micro Gas Turbine 2 Internal Flows 3 Ribbed Passage Flow & Heat Transfer Low Emission Combustor Rotor Dynamics & Bearing Diagnostics, Control & Measurement 2

Chairpersons: Chairpersons: Chairpersons: Chairpersons: Chairpersons: Chairpersons: Prof. Rene Van den Braembussch (von Karman Mr. Patrick Avran (Boyko Research-Engineering, Prof. Ryoichi S. Amano (University of Wisconsin- Prof. Francesco Martelli (University of Florence, Dr. Yasutomo Kaneko (Mitsubishi Heavy Prof. Giovanni Torella (Italian Airforce Academy, Institute, Belgium) France) Milwaukee, USA) Italy) Industries,Ltd.) Italy) Dr. Eito Matsuo (The University of Tokyo) Prof. Ken-ichi Funazaki (Iwate University) Prof. Takanari Okamura (Hachinohe Institute of Mr. Mitsuru Inada (Mitsubishi Heavy Industries,Ltd.) Mr. Kouichi Namba (Mitsui Engineering & Dr. Masahiro Kurosaki (Ishikawajima-Harima Heavy Technology) Shipbuilding Co., Ltd.) Industries Co.,Ltd.)

9:00 OS-104 TS-114 TS-078 TS-139 TS-017 TS-005 Numerical Analysis of 2.5 Dimensional Geometry Development of a New High-Speed Multi-Stage Rib-Induced Secondary Flow Structures inside a Intensification of Kinetic Combustion Performance Experimental Invesigation of 150 mm Diameter Detection and Prediction of the Performance Turbine Performance Compressor Facility ; Experimental Set Up High Aspect Ratio Trapezoidal Channel - in Hydrocarbon Fuels When the Oxidizing Large Hybrid Foil/Magnetic Bearing Deterioration of a Turbofan Engine Application to Cooling of Gas Turbine Blade Conversion Products are Used Trailing Edge - N. Watanabe (The University of Tokyo), S. D. Lippett (Cranfield University, United Kingdom), R. Kiml (Tokyo University of A&T), S. Mochizuki, A. V. V. Azatyan (Russian Academy of Sciences, H. Heshmat (Mohawk Innovative Technology, Inc., L. Marinai (Cranfield University, United Kingdom), Teramoto, T. Nagashima P. Timmis, P. Ivey, D. Bailey, G. Woollatt Murata, M. Sulitka Russia), G. K. Vedeshkin, E. D. Sverdlov USA), D. S. Xu R. Singh, B. Curnock, D. Probert

9:30 OS-105 TS-023 TS-079 TS-141 TS-018 TS-006 Some Aerodynamic Performances of Small Size Experimental Investigation on Shock Wave and PIV Flow Field Measurements in a Rotating U- Conical Flameholder with Pilot Burner for Lean Static and Dynamic Characteristics of High Speed Performance Analysis and Diagnostics of a Small Compressor and Turbine Stages Turbulent Boundary Layer Interactions in a Square Shaped Channel. Comparison of smooth and Premixed Combustion Multilobe Journal Bearings Gas Turbine Duct at Mach 2 and 4 90°rib-roughened walls. I.V. Gaydamaka (Central Institute of Aviation Motor, H. Sugiyama (Muroran Institute of Technology), K. Y. Servouze (Office National d‘Etudes et de T. Yamamoto (Japan Aerospace Exploration S. Strzelecki (Technical University of Lodz, Poland) J. Yin (Cranfield University, United Kingdom), M. S. Russia), A.V. Efimov, M.Ja. Ivanov, O.I. Ivanov, R.Z. Fukuda, K. Mizobata, L. Sun, R. Minato Recherches Aérospatiales, France), C. Brossard, Agency), Y. Kurosawa, S. Tachibana, S. Yoshida, Li, W. M. Huang Nigmatullin, N.I. Ogarko P. Gicquel K. Shimodaira, K. Suzuki 10:00 OS-106 TS-024 TS-080 TS-142 TS-019 TS-007 Structural Analysis of Rotating Parts of an Ultra- Computation of the Flow in a H.P.Compressor Heat Transfer Characteristic of a Triangular Injection of Lean Mixtures into Hot Burned Gas for Prototyping of Radial and Thrust Air Bearing for A Study on Applying Nonlinear Control to Gas micro Gas Turbine Drive Cone Cavity Channel with Turbulence Promoter Maintaining Low-NOx Emissions over an Extended Micro Gas Turbine Turbine Systems Range of Fuel-Air Ratios in Prevaporized Combustion M. Ishihama (Kanagawa Institute of Technology), Y. K. M. Tham (University of Sussex, United K. Takeishi (Mitsubishi Heavy Industries Ltd.), T. N. Aida (Hosei University), T. Nishijima, H. Yamada, S Kitazawa (The University of Tokyo), S. Kaneko, M. Ashikaga (Kawasaki Heavy Industries, Ltd.), Y. Sakai, K. Matsuzuki , T. Hikone Kingdom), C. A. Long, A. B. Turner, J. A. Dixon Kitamura, M. Matsuura, K, Shimizu S. Hayashi, T. Kawakami T. Watanabe Kohno, M. Higashi, K. Nagai , M. Ryu

10:30 OS-107 TS-025 TS-081 TS-135 TS-015 TS-153 Prototyping of Small-sized Two-dimensional Radial Experimental and Numerical Investigation of Effects of Rotation Speed on Heat Transfer in a Development of Low NOx Diffusive Burner Experimental Investigation into the Behavior of The Development of Operation System of a Liquid- Turbines Sealing Performance of Turbine Rim Seals 90°-Rib Roughened Two-Pass Duct Applying Spiral Flame Combustion Misaligned Shafts on Balanced Rotors fueled Micro Gas Turbine

K. Matsuura (The University of Tokyo), C. Kato, H. K. Teramachi (Ishikawajima-Harima Heavy Y. Y. Kim (Yonsei University, Korea), K. M. Kim, D. N. Hiromitsu (Ishikawajima Harima Heavy G. Hanish (Northumbria University, United Y. Mori (The University of Tokyo), S. Kaneko, T. Yoshiki, E. Matsuo, H. Ikeda, K. Nishimura, R. Industries Co., Ltd.), M. Hamane, T. Manabe, N. H. Rhee, H. H. Cho Industries Co., Ltd.), J. Hosoi, H. Toh , O. Kingdom), P. S. Leung, P. K. Datta Watanabe Sapkota Yanagidani Kawaguchi 11:00 TS-026 TS-082 TS-136 TS-016 TS-008 CFD Studies of Industrial Gas Turbine Exhaust The Effects of Oblique Discrete Rib Arrangement Characteristics of Low NOx Diffusion Combustion Dynamics of Asymmetric Rotors using Solid Numerical Correction of Pyrometry Data from Gas Diffusers on Heat Transfer Performance of a Square Duct with Strong Swirl Flow Models Turbines

K. Ishizaka (Mitsubishi Heavy Industries Ltd.), S. K. Tatsumi (Kyoto University), H. Iwai, K. Suzuki J. Yajima (Keio University), T. Hasegawa, O. J. S. Rao (Quality Engineering and Software J. Nickel (Technical University Berlin, Germany), H. Wakazono , M. Yuri , R. Takahashi Kawaguchi, N. Hiromitsu, J. Hosoi, H. Toh Technologies, India), R. Streenivas Pucher, M. Lüdtke

November 5 Wednesday 14:10 - 15:40 Organized Session 3 Session B-6 Session C-6 Session D-6 Session E-6 Ultra Micro Gas Turbine 3 Development & Verification of CFD codes Unsteady Flow & Noise 2 Conjugate Heat Transfer Analysis Performance Analysis of Gas Turbines: Intake Air Humidifying & Filtration

Chairpersons: Chairpersons: Chairpersons: Chairpersons: Chairpersons: Prof. Michael J. Ivanov (Central Institute of Aviation Dr. Hartmut Krain (DLR, Germany) Dr. Victor I. Mileshin (CIAM, Russia) Dr. Mike Wilson (University of Bath, UK) Prof. Wei Wang (Chinese Academy of Sciences, Motor, Russia) Prof. Nobuhiko Yamasaki (Kyushu University) Prof. Sadanari Mochizuki (Tokyo University of A&T) P.R.China) Prof. Chisachi Kato (The University of Tokyo) Mr. Eiichi Koda (Central Research Institute of Electric Power Industry)

14:10 OS-108 TS-020 TS-056 TS-083 TS-090 Concepts and Combustion Characteristics of a ｎ The Experience of CFD Calculations for Flow An Experimental Study on Unsteady Flow Conjugate Heat Transfer Analysis of a Test A Study of Performance on Advanced Humid Air Ultra-micro and a Micro Combustor Analysis in Centrifugal Compressor Stages Behaviors in an Axial-Flow Turbine Configuration for a Film-cooled Blade Turbine Systems

S. Yuasa (Tokyo Metropolitan Institute of Y. B. Galerkin (TU Saint-Petersburg, Russia), V. P. S. Kasuga (Tokyo Denki University), A. Yamamoto, K. Kusterer (Aachen University, Germany), D. E. S. Higuchi (Hitachi, Ltd.), S. Hatamiya, N. Seiki, S. Technology), K. Oshimi, M. Uehara Mitrofanov, A. Y. Prokofiev T. Miyachi, T. Okaniwa Bohn , T. Sugimoto, R. Tanaka Marushima

14:40 OS-109 TS-021 TS-057 TS-084 TS-091 Internal Heat Mixing and External Heat Losses in Numerical Prediction of Humid Effect to Transonic Wake Decay within the Stator Vane in a High- Numerical Parametric Study on Full Coverage High Fogging Tests and Performance Model for an Ultra Micro Turbine Flows in Turbomachinery Speed Axial-Flow Compressor Cooled Multi-Layer Plates High Fogging

Y. Ribaud (ONERA, France) Y. Sasao (Tohoku University), S. Yamamoto R. Nohara (Ishikawajima-Harima Heavy Industries D. E. Bohn (Aachen University, Germany), N. J. Hoffmann (Alstom (Schweiz) AG, Switzerland), Co.,Ltd.), K. Imanari, I. Fujii, Y. Ooba Moritz C. Ojo

15:10 OS-110 TS-022 TS-058 TS-085 TS-092 Performance of a Micro-scale Radial-Flow High Accuracy Multigrid Method of the Unsteady Effects of Airfoil Clocking on Aero-performance Conjugate Simulations of Flow and Heat Outstanding Operational Behavior of Taylor-Made Compressor Impeller Made of Silicon Nitride Convection Diffusion Equation and Calculations of and Unsteady Blade Loading in a High-Speed Conduction for Turbine Cooling Nonwovens Filters for Intake Air Filtration of Gas Heat and Fluid Flow Axial Compressor Turbines

J. P. Johnston (Stanford University, USA), S. Kang, W. Wu (The University of Shanghai for Science and D. Kato (Ishikawajima-Harima Heavy Industries T. Yamane (Japan Aerospace Exploration Agency), M. Schmidt (Freudenberg & Vilene Nonwovens T. Arima, M. Matsunaga, H. Tsuru, F. B. Prinz Technology, P.R.China) , Y. Ge Co., Ltd.), K. Imanari F. Mimura, T. Yoshida, S. Yamawaki, C. Nakamata, (Suzhou) Co., Ltd., P.R.China), S. Berbner, A. R. Imai Klink, M. Waldenmaier, R. Schulz

3 As of Oct. 17, 2003 November 6 Thursday 9:00 - 11:00 Speaker's Name is underlined. Organized Session 4 Session B-7 Session C-7 Session D-7 Session E-7 Session F-7 Marine Gas Turbines & Turbocharger Surge/Stall 1 Industrial Gas Turbine & Power Plant 1 Impingement & Film Cooling Combustor Design Performance Analysis of Gas Turbines & New Systems

Chairpersons: Chairpersons: Chairpersons: Chairpersons: Chairpersons: Chairpersons: Mr. Katsuhide Hiraoka (National Maritime Research Prof. Frans A.E. Breugelmans (von Karman Mr. Masafumi Fukuda (Toshiba Corporation) Dr. Boris Kurmanov (ALSTOM Power Uniturbo, Dr. Shigeru Hayashi (Japan Aerospace Exploration Dr. Juergen Hoffmann (Alstom (Schweiz) AG, Institute) Institute, Belgium) Mr. Toshiyuki Takagi (Mitsui Engineering & Russia) Agency) Switzerland) Mr. Masatoshi Chiba (Ishikawajima-Harima Heavy Prof. Yutaka Ohta (Waseda University) Shipbuilding Co., Ltd.) Dr. Toyoaki Yoshida (Japan Aerospace Exploration Dr. Hidemi Toh (Ishikawajima-Harima Heavy Dr. Hideto Moritsuka (Central Research Institute of Industries Co.,Ltd.) Agency) Industries Co.,Ltd.) Electric Power Industry)

9:00 OS-201 TS-037 TS-098 TS-074 TS-143 TS-086 Turbocharger Technology for Personal Water Craft A Stability Model for Transonic Axial Compressors High-efficiency Gas Turbines Operating in Jet Impingement onto a Dimpled Surface with Investigation of Cooling Structure with MGC A Comparative Investigation of Reheat in Gas Intermediate Duty Different Crossflow Schemes Material for a High Temperature Gas Turbine Turbine Cycles Combustor Y. Matsuyama (Ishikawajimaharima Heavy W. Yu (Beijing University of Aeronautics and B. Becker (SIEMENS POWER GENERATION, K. Kanokjaruvijit (Imperial College London, United T. Hagari (Kawasaki Heavy Industries, Ltd.), K. K. Sarabchi (University of Tabriz, Iran) Industries CO., LTD.), H. Furukawa, T. Mineta, T. Astronautics, P.R.China), X. Sun Germany), V. Thien Kingdom), R. F. Martinez-Botas Ishida, Y. Kinoshita Fukuda 9:30 OS-202 TS-038 TS-099 TS-075 TS-144 TS-087 Research and Development of Gas Turbine for Prediction and Active Control of Surge Inception of Modernization and Upgrade Programs for Enhanced Impingement Heat Transfer: Effect of Primary Equivalence Ratio on Reducing A Novel LNG and Oxygen Stoichiometric Next-Generation Marine Propulsion System (Super a Centrifugal Compressor Mitsubishi Heavy-duty Gas Turbines Comparison of Co-flow and Cross-flow with Rib both Fuel-NOx and Thermal-NOx Emissions of the Combustion Cycle without CO ₂ Emission Marine Gas Turbine) Turbulators Gas Turbine Combustor for Oxygen-blown IGCC with Hot/Dry Syngas Cleanup M. Arai (Technological Research Association of N. Hagino (Kanagawa Institute of Technology), K. K. Watanabe (Mitsubishi Heavy Industries, Ltd.), H. G. E. Andrews (The University of Leeds, United T. Hasegawa (Central Research Institute of Electric W. Wang (Chinese Academy of Sciences, Super Marine Gas Turbine), T. Sugimoto, K. Imai Uda, Y. Kashiwabara Arimura, K. Akagi, H. Sakuma Kingdom), R.A.A. Abdul Hussain , M. C. Mkpadi Power Industry), M. Sato P.R.China), R. Cai, N. Zhang, H. Jin ,H. Miyaji, K. Nakanishi, Y. Hamachi 10:00 OS-203 TS-039 TS-100 TS-076 TS-145 TS-089 The WR-21 Intercooled Recuperated Gas Turbine The Measurements of Unsteady Flow Fields in an Development and In-house Shop Load Test Heat Transfer in Impingement/Effussion Cooling Numerical/Experimental Methodology for the Off-Design Analysis of the GRAZ Cycle Engine- Integration Into Future Warships Axial Flow Fan under Stalled Condition Results of M701G2 Gas Turbine System with Rib Turbulators Retrofitting of Combustion Chambers for Gas Performance Turbines C. R. English (Royal Navy, United Kingdom) K. H. Kim (Korea Institute of Science and A. Maekawa (Mitsubishi Heavy Industries, LTD.), R. Y. W. Nam (Yonsei University, Korea), D. H. Rhee, F. Martelli (The University of Florence, Italy), G. A. Miller (Warsaw University of Technology, Technology, Korea) , Y. H. Shin, C. S. Kang Magoshi, Y. Iwasaki H. H. Cho Riccio, P. Adami, G. Benelli, G. Tanzini Poland), J. Lewandowski, K. Badyda, S. Kiryk, J. Milewski, J. Hama, N. Iki 10:30 OS-204 TS-040 TS-077 TS-134 Rolls-Royce MT30 Design, Certification, Launch Development of a Surge Prediction System for Experimental Investigation on Heat Transfer and Numerical Prediction of Turbulent Combustion and Growth Multi Stage Axial Compressors Film Cooling of High Loaded Transonic Turbine Flows in Staged Combustor Using LES and Vanes and Blades Extended G-Equation

S. Wilmshurst (Rolls-Royce plc, United Kingdom) H. Hoenen (RWTH Aachen University, Germany), R. Nogami (Mitsubishi Heavy Industries, LTD.), K. T. Tominaga (The University of Tokyo), Y. Itoh, N. T. Arnold Shimizu, K. Takeishi, T. Kitamura Taniguchi, T. Kobayashi, T. Hagari, Y. Nonaka

November 6 Thursday 13:30 - 15:00 Session A-8 Session B-8 Session C-8 Session D-8 Session E-8 Session F-8 Force/Vibration Surge/Stall 2 Industrial Gas Turbine & Power Plant 2 Flows in Rotating or Bended Duct Optimization & Inverse Method Performance Analytic Modellings & Tool

Chairpersons: Chairpersons: Chairpersons: Chairpersons: Chairpersons: Chairpersons: Dr. Herwart T. Hoenen (RWTH Aachen University, Prof. Yasushige Kashiwabara (Kanagawa Institute Dr. Bernard Becker (SIEMENS POWER Prof. Dieter Bohn (Aachen University, Germany) Dr. David C. Wisler (GE Aircraft Engines, USA) Mr. Stewart Wilmshurst (Rolls-Royce plc, UK) Germany) of Technology) GENERATION, Germany) Dr. Kenichiro Takeishi (Mitsubishi Heavy Dr. Hidekazu Kodama (Ishikawajima-Harima Heavy Dr. Tadaharu Kishibe (Hitachi Ltd.) Dr. Dai Kato (Ishikawajima-Harima Heavy Dr. Shinya Marushima (Hitachi Ltd.) Industries,Ltd.) Industries Co.,Ltd.) Industries Co.,Ltd.)

13:30 TS-053 TS-044 TS-101 TS-063 TS-034 TS-093 Study on Blade Forced Vibration Response of Early Pre-stall Investigation by Sensitive Stall Repowering of Lowshan Power Plant Pressure Loss Characteristics in Rotating Coolant New Quasi-3D Inverse Navier-Stokes Based Thermodynamic Table for Performance Radial Inflow Turbine Warning Technique Passages of Gas Turbine (Effect of Inlet Flow Method Used to Design Highly Loaded Axial Calculations in Gas Turbine Engine Angle in Intermediate Shaft) Compressor Stages K. Nakano (Ishikawajima-Harima Heavy Industries N. Tahara (Ishikawajima-Harima Heavy Industries M. R. Shahnazari (Niroo Research Institute, Iran), H. Matsuda (TOSHIBA Corporation), F. Otomo, A. V. I. Mileshin (Central Institute of Aviation Motors, M. Iwai (Shenyang Institute of Aeronautical Co. Ltd), H. Hattori, Y. Hirata Co.,Ltd.), M. Kurosaki , Y. Ohta , E. Outa , H. D. Foroughi, H. Fakharian Inomata, K. Kitayama, Y. Fukuyama Russia), S. K. Shchipin, A. N. Startsev Engineering, China) Shinohara 14:00 TS-054 TS-045 TS-102 TS-064 TS-035 TS-094 Euler/N-S Analysis of Linear Unsteady Experimental Investigation of Rotating Stall Gas Turbine Based Power Plants Repowering Effects of Swirl and Flow Rate on the Flow and Geometry Optimization of Turbine Blade with Low Bypass Ratio Turbofan Performance Aerodynamic Forces on Vibrating Annular Inception in Axial Flow Fans Reduces Emissions and Increase Efficiency of Heat Transfer in a Pre-swirl Rotating-disc System Surface Injection Modelling with Fan Radial Flow Profiles Cascade Existing Plants while Re-utilising Available Assets T. Nagasaki (Kyushu University), N. Yamasaki S.K.Sane (Indian Institute of Technology Bombay, H. -R. Schenk (ALSTOM), G. Ehren, Yu TatMing M. Farzaneh-Gord (University of Bath, United T. Nagumo (Tokyo University of Science), K. Toda, M. S. Li (Cranfield University, United Kingdom), J. India), D. Sekhar, N. V. Patil, P. Tagade Kingdom), M. Wilson, J. M. Owen M. Yamamoto F. Yin, B. Curnock

14:30 TS-055 TS-046 TS-103 TS-065 TS-036 TS-095 Numerical Analysis of Active Cascade Flutter Unsteady Phenomena during Transient Process in Design for F Class Blast Furnace Gas Firing 300 Predictions of a Turbulent Flow Inside a Sharp U- The Development of a Genetic Algorithm Code for An Improved Analytic Model to Predict Fouling Control with Smart Structure Radial Vanelss Diffuser MW Gas Turbine Combined Cycle Plant Curve Duct for a Turbine Blade Cooling Passage Secondary Flow Injection Optimization in Axial Phenomena in the Axial Compressor of Gas Turbines Turbine Engines J. Kazawa (The University of Tokyo), T. Watanabe N. Hayashi (Chiba Institute of Technology), T. T. Komori (Mitsubishi Heavy Industries, Ltd.), H. R. S. Amano (University of Wisconsin-Milwaukee, C. F. F. Favaretto (Iwate University), K. Funazaki, T. T. W. Song (Seoul National University, Korea), J. L. Tagawa, M. Koyama, I. Ariga, M. Sano Hara, H. Arimura, Y. Kitauchi USA), B. Song Tanuma Sohn, T. S. Kim, J. H. Kim, S. T. Ro

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