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Papers
Conference Year Paper Title Paper Author Page Number Other
IGTI  2000  A Probabilistic Approach to Aeropropulsion System Assessment  Michael T. Tong, NASA Glenn Research Center, Cleveland, OH, USA    2000-GT-0001 
IGTI  2000  GSP, A Generic Object-Oriented Gas Turbine Simulation Environment  Wilfried P.J. Visser, Michael J. Broomhead, National Aerospace Laboratory, Amsterdam, The Netherlands    2000-GT-0002 
IGTI  2000  The Use of Variable Fidelity Models in the Optimization Problems for Aircraft Engines Parameters and Control Laws  I.N. Egorov, G.V. Kretinin, I.A. Leshchenko, Air Force Engineering Academy, Moscow, Russia; Y.I. Babiy, "Techno-Pulsar" Company, Moscow, Russia    2000-GT-0003 
IGTI  2000  Re-Designing Annular Combustor of APU for Better Air Management and Spray Development  Petr Cízek, Miroslav Jícha, Brno University of Technology, Brno, Czech Republic    2000-GT-0004 
IGTI  2000  Implementation of a Compressor Face Boundary Condition Based on Small Disturbances  John W. Slater, John H. Glenn Research Center at Lewis Field, Cleveland, OH, USA; Gerald C. Paynter, The Boeing Company, Seattle, WA, USA    2000-GT-0005 
IGTI  2000  A New Compressor Map Scaling Procedure for Preliminary Conceptional Design of Gas Turbines  Joachim Kurzke, Claus Riegler, MTU München GmbH, München, Germany    2000-GT-0006 
IGTI  2000  The Gas Turbine Test Facility in the Information Age  Grant T. Patterson, C. Edward Dorman, W. R. Sloan, Sverdrup Technology, Inc., Arnold Air Force Base, TN, USA    2000-GT-0007 
IGTI  2000  A.R. Howell - Father of the British Axial Compressor  John Dunham, PCA Engineers Ltd., Lincoln, England, UK    2000-GT-0008 
IGTI  2000  The Last 1/3  David M. Carpenter, Jet Pioneer of America, Danvers, MA, USA    2000-GT-0009 
IGTI  2000  Propulsion System Integration of Turboprop Aircraft for Basic Trainer  Changduk Kong, Chosun University, Kwangju, Korea    2000-GT-0010 
IGTI  2000  Steady Performance Measurements of a Turbofan Engine with Inlet Distortions Containing Co- and Counter-Rotating Swirl from an Intake Diffuser for Hypersonic Flight  Norbert R. Schmid, Dirk C. Leinhos, Leonhard Fottner, Universität der Bundeswehr München, Neubiberg, Germany    2000-GT-0011 
IGTI  2000  NASA's HSCT - Past and Future Prospects  Robert A. Mercure, NASA Headquarters, Washington, DC, USA    2000-GT-0012 
IGTI  2000  Demonstration of Fluidic Throat Skewing for Thrust Vectoring in Structurally Fixed Nozzles  Patrick J. Yagle, Daniel N. Miller, K. Brant Ginn, Jeffrey W. Hamstra, Lockheed Martin Tactical Aircraft Systems, Fort Worth, TX, USA    2000-GT-0013 
IGTI  2000  The Potential Impact of Utilizing Advanced Engine Technology for a Combat Capable Unmanned Air Vehicles (UAV)  Greg B. Bruening, Air Force Research Laboratory, Wright-Patterson Air Force Base, OH, USA; James R. Snyder, Raymond E. Fredette, Universal Technologies Corporation, Dayton, OH, USA    2000-GT-0014 
IGTI  2000  Study of an External Fired Gas Turbine Power Plant Fed by Solid Fuel  G. Riccio, F. Martelli, S. Maltagliati, University of Florence, Florence, Italy    2000-GT-0015 
IGTI  2000  Thermodynamic Performance Analysis and Economic Evaluation of Externally Fired Gas Turbine Cycles for Small Scale Biomass Cogeneration  Marie Anheden, Andrew Martin, Royal Institute of Technology, Stockholm, Sweden    2000-GT-0016 
IGTI  2000  Concepts for the Production of Biomass Derived Fuel Gases for Gas Turbine Applications  W. Schmitz, D. Hein, Technische Universität München, Munich, Germany    2000-GT-0018 
IGTI  2000  An Analysis of the Potential for Deposition, Erosion, or Corrosion in Gas Turbines Fueled by the Products of Biomass Gasification or Combustion  I.G. Wright, C. Leyens, B.A. Pint, Oak Ridge National Laboratory, Oak Ridge, TN, USA    2000-GT-0019 
IGTI  2000  Integration of Advanced Gas Turbines in Pulp and Paper Mills for Increased Power Generation  Katarina Maunsbach, Anna Isaksson, Jinyue Yan, Gunnar Svedberg, Royal Institute of Technology, Stockholm, Sweden; Lars Eidensten, Vattenfall Utveckling AB, Stockholm, Sweden    2000-GT-0020 
IGTI  2000  Simulation of Steam-Based Gasification Processes for Topping Combustion in the Biomass Air Turbine (BAT) Cycle  Jens Wolf, Jinyue Yan, Royal Institute of Technology, Stockholm, Sweden    2000-GT-0021 
IGTI  2000  Biomass-Based, Small-Scale, Distributed Generation of Electricity and Heat Using Integrated Gas Turbine-Fuel Cell Systems  B.J.P. Buhre, J. Andries, Delft University of Technology, Delft, The Netherlands    2000-GT-0022 
IGTI  2000  Performance of a Biomass Integrated Gasification Combined Cycle CHP Plant Supplying Heat to a District Heating Network  Simon Harvey, Chalmers University of Technology, Göteborg, Sweden    2000-GT-0023 
IGTI  2000  Combined Cycles for High Performance, Low Cost, Low Environmental Impact Waste-to-Energy Systems  Stefano Consonni, Politecnico di Milano, Milan, Itlay    2000-GT-0024 
IGTI  2000  Feedstock Blending in a Continuously Fed Gasifier  Greg P. Schaefer, Alex E.S. Green, University of Florida, Gainesville, FL, USA    2000-GT-0025 
IGTI  2000  Operation Experiences of Siemens IGCC Gas Turbines Using Gasification Products from Coal and Refinery Residues  M. Huth, A. Heilos, G. Gaio, J. Karg, Siemens AG Power Generation Group (KWU), Mülheim, Germany    2000-GT-0026 
IGTI  2000  Integration of High Performance Power Systems (HIPPS) into Vision 21  Fred L. Robson, kraftWork Systems, Inc., Amston, CT, USA; John D. Ruby, Bechtel National, Inc., San Francisco, CA, USA; Dr. Daniel J. Seery, United Technologies Research Center, East Hartford, CT, USA    2000-GT-0027 
IGTI  2000  Development of Low NOx Combustion Technology in Medium-Btu Fueled 1300 °C - class Gas Turbine Combustor in IGCC  Takeharu Hasegawa, Tohru Hisamatsu, Yasunari Katsuki, Mikio Sato, Central Research Institute of Electric Power Industry, Kanagawa, Japan    2000-GT-0028 
IGTI  2000  An Evaluation of Engine Faults Diagnostics Using Artificial Neural Networks  Pong-Jeu Lu, Tzu-Cheng Hsu, National Cheng Kung University, Tainan, Taiwan; Ming-Chuan Zhang, Jin Zhang, Beijing University of Aeronautics and Astronautics, Beijing, China    2000-GT-0029 
IGTI  2000  Advanced Diagnostics and Prognostics for Gas Turbine Engine Risk Assessment  Michael J. Roemer, Gregory J. Kacprzynski, Impact Technologies, LLC, Rochester, NY, USA    2000-GT-0030 
IGTI  2000  Designing Diagnostic Expert Systems for Long-Term Supportability  Graham Forsyth, DSTO, Victoria, Australia; John Delaney, Competitive Advantage Technology Pty Ltd. and eVision Pty Ltd, Victoria, Australia    2000-GT-0031 
IGTI  2000  An Investigation of Artificial Neural Network (ANN) in Quantitative Fault Diagnosis for Turbofan Engine  Sun Bin, Zhang Jin, Beijing University of Aeronautics and Astronautics, Beijing, China; Zhang Shaoji, Shenyang Aeroengine Research Institute, Shenyang, China    2000-GT-0032 
IGTI  2000  Identifying Faults in the Variable Geometry System of a Gas Turbine Compressor  A. Tsalavoutas, K. Mathioudakis, A. Stamatis, National Technical University of Athens, Athens, Greece; M. Smith, ABB Alstom Power UK Ltd, Lincoln, UK    2000-GT-0033 
IGTI  2000  Combining Advanced Data Analysis Methods for the Constitution of an Integrated Gas Turbine Condition Monitoring and Diagnostic System  A. Tsalavoutas, N. Aretakis, K. Mathioudakis, A. Stamatis, National Technical University of Athens, Athens, Greece    2000-GT-0034 
IGTI  2000  Neural Networks Based Diagnostics for Mistuned Bladed Disk  Pei-Yuan Peng, United Technologies Research Center, East Hartford, CT, USA; M. T. Yang, Pratt & Whitney, Middletown, CT, USA    2000-GT-0035 
IGTI  2000  Neural Network Modeling of Turbofan Engine Parameters  Mark J. Embrechts, Rensselaer Polytechnics Institute, Troy, NY, USA; Aaron L. Schweizerhof, Mark Bushman, Mike H. Sabatella, Pratt & Whitney, East Hartford, CT, USA    2000-GT-0036 
IGTI  2000  Performance of Gas Turbine Power Plants Controlled by One Step Ahead Adaptive Technique  L. Dambrosio, B. Fortunato, Polytechnic University of Bari, Italy; S.M. Camporeale, University of Reggio Calabria, Italy    2000-GT-0037 
IGTI  2000  Performance Seeking Control of Regenerative Gas Turbine Engines  Nanahisa Sugiyama, National Aerospace Laboratory, Tokyo, Japan    2000-GT-0038 
IGTI  2000  Implementation of a Multivariable Control  Louis J. Larkin, James Philpott, Pratt & Whitney Engineering, West Palm Beach, FL, USA    2000-GT-0039 
IGTI  2000  Nonlinear Model Predictive Control Experiments on a Laboratory Gas Installation  H.A. van Essen, H.C. de Lange, Eindhoven University of Technology, Eindhoven, The Netherlands    2000-GT-0040 
IGTI  2000  Advanced Fuel Metering for Aero Engines  Freidrich Schwamm, DaimlerChrysler, München, Germany    2000-GT-0041 
IGTI  2000  An Object-Oriented Program for the Dynamic Simulation of Gas Turbines  M. Agresti, B. Fortunato, Polytechnic University of Bari, Bari, Italy; S.M. Camporeale, University of Reggio Calabria, Reggio Calabria, Italy    2000-GT-0042 
IGTI  2000  ZP/LTR Control for Turbofan Engines  Zhengping Feng, Shanghai Jiaotong University, Shanghai, China; Jianguo Sun, Qiuhong Li, Nanjing University of Aeronautics and Astronautics, Nanjing, China    2000-GT-0043 
IGTI  2000  Gas Turbine Mach Number Control with Simplified Fuel System  Graham J. Dadd, Defence Research and Evaluation Agency, Hampshire, UK; Kin K. Chan, Frazer-Nash Consultancy Ltd., Surrey, UK    2000-GT-0044 
IGTI  2000  Design and Test of a Semi-Passive Flow Control Device for Inlet Distortion Suppression  Link C. Jaw, Dong N. Wu, David J. Bryg, Scientific Monitoring, Inc., Tempe, AZ, USA; William T. Cousins, Honeywell International, Phoenix, AZ, USA    2000-GT-0045 
IGTI  2000  Fuzzy Fuel Flow Selection Logic for a Real Time Embeded Full Authority Digital Engine Control  Angelo Martucci, Allan Volponi, Hamilton Sundstrand, Winsdor Locks, CT    2000-GT-0046 
IGTI  2000  Closed Loop Minimisation of NOx Emissions in a Gas Turbine  Ravi Rajamani, George Goodman, John Bolton, GE Corporate Research & Development, Schenectady, NY, USA; Narendra Joshi, Rick Hook, Eric Kress, Bill Barrow, GE Aircraft Engines, Evendale, OH, USA    2000-GT-0047 
IGTI  2000  The Use of Hot-Wire Anemometry to Investigate Unsteady Wake-Induced Boundary-Layer Development on a High Lift LP Turbine Cascade  Stefan Wolff, Stefan Brunner, Leonhard Fottner, Universität der Bundeswehr München, Neubiberg, Germany    2000-GT-0049 
IGTI  2000  Structural Health Monitoring with Piezoelectric Active Sensors  Howard A. Winston, Fanping Sun, Balkrishna S. Annigeri, United Technologies Research Center, East Hartford, CT, USA    2000-GT-0051 
IGTI  2000  Evaluation of an Uncooled Focal Plane Array Infrared Camera for Effusion Cooling Research  Scott K. McGhee, A.M. Birk, Queen's University, Kingston, ON, Canada    2000-GT-0052 
IGTI  2000  A Fiber-Optic Tip-Shroud Deflection Measurement System  Rudy A. Rooth, Wiebren Hiemstra, KEMA Nederland B.V., Arnhem, The Netherlands    2000-GT-0053 
IGTI  2000  Syncronized LDV Measurement in Centrifugal Impeller: Seeding Insemination Set Up and CFD Comparison  M. De Lucia, C.P. Mengoni, P. Boncinelli, University of Florence, Florence, Italy; U. Corradini, GE-Nuovo Pignone, Florence, Italy    2000-GT-0054 
IGTI  2000  Experimental Investigation of the Blade-to-Blade Flow in a Compressor Rotor by Digital Particle Image Velocimetry  N. Balzani, F. Scarano, M.L. Riethmuller, F.A.E. Breugelmans, Von Karman Institute for Fluid Dynamics, Rhode-St.-Genèse, Belgium    2000-GT-0055 
IGTI  2000  Application of Incomplete Measurement Data to Thermal Diagnostics of Complex Power Systems Components  Jerzy Gluch, Jerzy Krzyzanowski, Polish Academy of Sciences, Gdansk, Poland    2000-GT-0056 
IGTI  2000  Application of On-Line Optimization Technology to Plant Operation  Rodney R. Gay, GE Enter Software, Davis, CA, USA    2000-GT-0058 
IGTI  2000  Understanding Machinery Management - Using Machine Condition and Process Information for Maximum Benefit  Roger G. Harker, Bently Nevada Corporation, Minden, NV, USA    2000-GT-0059 
IGTI  2000  X-Ray Refraction Characterization of the Interface Structure of Ceramics  Manfred P. Hentschel, Karl-Wolfram Harbich, Joerg Schors, Axel Lange, Federal Institute for Materials Research & Testing, Berlin, Germany    2000-GT-0061 
IGTI  2000  Slow Crack Growth Analysis of Advanced Structural Ceramics Under Combined Loading Conditions - Damage Assessment in Life Prediction Testing  Sung R. Choi, Ohio Aerospace Institute, Cleveland, OH; John P. Gyekenyesi, NASA Glenn Research Center, Cleveland, OH    2000-GT-0062 
IGTI  2000  Predicting the Deterministic Effects of Combustion Gas Environments on the Stress-Rupture Life of Silicon Nitride Turbine Components  Thomas E. Strangman, Bjoern Schenk, Honeywell Engines & Systems, Phoenix, AZ, USA    2000-GT-0063 
IGTI  2000  Finite Element Analysis of the Critical Flaw Size in Hybrid Silicon Nitride Bearing Ball  Sunil G. Warrier, David C. Jarmon, United Technologies Research Center, East Hartford, CT, USA; Herbert A. Chin, Pratt & Whitney, West Palm Beach, FL, USA    2000-GT-0065 
IGTI  2000  Modeling the Tensile Behaviour of a SiC/SiC Composite by Master Curves  J. Shi, ABB ALSTOM Technology Centre, Leicester, UK    2000-GT-0066 
IGTI  2000  Development of Continuous Fiber Reinforced Reaction Sintered Silcon Carbide Matrix Composite for Gas Turbine Hot Parts Application  Tsuneji Kameda, Yoshiyasu Itoh, Tsuneo Hijikata, Takanari Okamura, Toshiba Corporation, Yokohama, Japan    2000-GT-0067 
IGTI  2000  Characterization of Melt-Infiltrated SiC/SiC Composite Combustor Liners Using Meso- and Micro- NDE Techniques  W.A. Ellingson, J.G. Sun, Argonne National Laboratory, Argonne, IL, USA; K.L. More, Oak Ridge National Laboratory, Oak Ridge, TN, USA; R. Hines, BF Goodrich, Inc., Santa Fe Springs, CA, USA    2000-GT-0068 
IGTI  2000  Design, Fabrication, and Testing of Ceramic Joints for High Temperature SiC/SiC Composites  M. Singh, Dynacs Engineering Co., Cleveland, OH, USA; Edgar Lara-Curzio, Oak Ridge National Laboratory, Oak Ridge, TN, USA    2000-GT-0069 
IGTI  2000  Design, Analysis, Fabrication and Testing of a CMC Combustor Can  Jun Shi, ABB Alstom Power Technology Centre, Leicester, UK    2000-GT-0071 
IGTI  2000  SiC Fiber Reinforced Ceramic Matrix Composites for Turbine Engine Applications  Kenneth Hatton, Dennis Landini, Stan Hemstad, Honeywell Advanced Composites Inc., Newark, DE, USA; R. Craig Robinson, Dynacs Aerospace Company, Inc., Brook Park, OH, USA    2000-GT-0072 
IGTI  2000  Ceramic Vanes for a Model 501-K Industrial Turbine Demonstration  Richard A. Wenglarz, Ken Kouns, Rolls-Royce Allison, Indianapolis, IN, USA    2000-GT-0073 
IGTI  2000  Ceramic Gas-Turbine 2.5 MW Engine for Gas Industry Application in Russia  A.V. Soudarev, A.A. Souryaninov, V.V. Grishaev, V. Ya. Podgorets, V. Yu. Tikhoplav, B.V. Soudarev, Research-Engineering Centre, St. Petersburg, Russia    2000-GT-0074 
IGTI  2000  Ceramic Stationary Gas Turbine Development Program - Seventh Annual Summary -  Jeffrey Price, Oscar Jimenez, Vijay Parthasarathy, Narendernath Miriyala, Don Leroux, Solar Turbines Incorporated, San Diego, CA, USA    2000-GT-0075 
IGTI  2000  Recommended Direction of the Solar/DOE Ceramic Stationary Gas Turbine Program  S. Gates, Jr., J. Price, V. Parthasarathy, N. Miriyala, O. Jimenez, Solar Turbines Incorporated, San Diego, CA, USA    2000-GT-0076 
IGTI  2000  Chemical Vapour Deposition of TBC: An Alternative Process for Gas Turbine Components  G. Wahl, W. Nemetz, IOPW, Braunschweig, Germany; M. Giannozzi, Nuovo Pignone, Florence, Italy; S. Rushworth, EPICHEM, Bromborough, Great Britain; D. Baxter, IAM JRC, Petten, Netherlands; N. Archer, ATL, Uycomb, Great Britain; F. Cernuschi, ENEL Ricerca, M    2000-GT-0077 
IGTI  2000  Suppression of Dynamic Combustion Instabilities by Passive and Active Means  Peter Berenbrink, Stefan Hoffmann, Siemens AG, KWU, Muelheim, Germany    2000-GT-0079 
IGTI  2000  Investigation of Cycle-to-Cycle Variability in an Unstable Gas Turbine Combustor  Tim C. Lieuwen, Ben T. Zinn, Georgia Institute of Technology, Atlanta, GA, USA    2000-GT-0081 
IGTI  2000  Influence of the Combustor Aerodynamics on Combustion Instabilities from Equivalence Ratio Fluctuations  Thomas Sattelmayer, Technische Universität München, Garching, Germany    2000-GT-0082 
IGTI  2000  The Effect of Fuel/Air Mixing on Actuation Authority in an Active Combustion Instability Control System  Jeffrey M. Cohen, John H. Stufflebeam, William Proscia, United Technologies Research Center, East Hartford, CT, USA    2000-GT-0083 
IGTI  2000  Experimental Investigations of the Temporal Air-Fuel Mixing Fluctuations and Cold Flow Instabilities of a Premixing Gas Turbine Burner  K.-U. Schildmacher, R. Koch, S. Wittig, University of Karlsruhe, Karlsruhe, Germany; W. Krebs, S. Hoffmann, Siemens AG, Mülheim, Germany    2000-GT-0084 
IGTI  2000  Reduced NOx Diffusion Flame Combustors for Industrial Gas Turbines  Alan S. Feitelberg, Venkat E. Tangirala, GE Corporate Research and Development, Niskayuna, NY, USA; Richard A. Elliott, Roointon E. Pavri, Richard B. Schiefer, GE Power Systems, Schenectady, NY, USA    2000-GT-0085 
IGTI  2000  9 PPM NOx/CO Combustion System for "F" Class Industrial Gas Turbines  Christian L. Vandervort, Ph.D., P.E., GE Power Systems, Schenectady, NY, USA    2000-GT-0086 
IGTI  2000  A High-Temperature Catalytic Combustor with Starting Burner  Yusaku Yoshida, Kenshun Oyakawa, Japan Automobile Research Institute, Inc., Ibaraki, Japan; Yukio Aizawa, Nippon Mitsubishi Oil Co., Yokohama, Kanagawa, Japan; Hiroshi Kaya, Tonen Co., Tokyo, Japan    2000-GT-0087 
IGTI  2000  Field Demonstration of a 1.5 MW Industrial Gas Turbine with a Low Emissions Catalytic Combustion System  David K. Yee, Kare Lundberg, Chris K. Weakley, Catalytica Combustion Systems, Inc., Mountain View, CA, USA    2000-GT-0088 
IGTI  2000  Experience of Environmental Update of Gas-Pumping Units  A. Soudarev, E. Vinogradov, Yu. Zakharov, EST, St.-Petersburg, Russia; K.-H. Scholz, E. Zizow, Ruhrgas AG, Essen, Germany; S. Vesely, S. Paryzek, EKOL, Brno, Czech Republic    2000-GT-0089 
IGTI  2000  Determination of Thermoacoustic Response in a Demonstrator Gas Turbine Engine  C.A. Arana, B. Sekar, Air Force Research Laboratory, Wright Patterson AFB, OH, USA; M.A. Mawid, Engineering Research & Analysis Co., Dayton, OH, USA    2000-GT-0091 
IGTI  2000  Velocity Measurements in a Combustor Undergoing Limit-Cycle Pressure Oscillations  J. Li, S. Acharya, Louisiana State University, Baton Rouge, LA, USA    2000-GT-0092 
IGTI  2000  Experimental Replication of an Aeroengine Combustion Instability  J.M. Cohen, J.R. Hibshman, W. Proscia, T.J. Rosfjord, B.E. Wake, United Technologies Research Center, East Hartford, CT, USA; J.B. McVey, jbScienceS, Glastonbury, CT, USA; J. Lovett, M. Ondas, Pratt & Whitney, West Palm Beach, FL, USA; J. DeLaat, K. Breis    2000-GT-0093 
IGTI  2000  Acoustic Resonances of an Industrial Gas Turbine Combustion System  S. Hubbard, A.P. Dowling, University of Cambridge, Cambridge, UK    2000-GT-0094 
IGTI  2000  Prediction and Measurement of Thermoacoustic Improvements in Gas Turbines with Annular Combustion Systems  Uwe Krüger, Jens Hüren, B&B-AGEMA, Aachen, Germany; Stefan Hoffmann, Werner Krebs, Patrick Flohr, Siemens AG, Mülheim, Germany; Dieter Bohn, Aachen University of Technology, Aachen, Germany    2000-GT-0095 
IGTI  2000  Infrared Measurements of Thermoacoustic Instabilities in a Swirl-Stabilized Combustor  D. Allgood, S. Murugappan, S. Acharya, E. Gutmark, Louisiana State University, Baton Rouge, LA, USA    2000-GT-0096 
IGTI  2000  Pressure Effect on NOx and CO Emissions in Industrial Gas Turbines  Anuj Bhargava, Donald W. Kendrick, Meredith B. Colket, William A. Sowa, United Technologies Research Center, East Hartford, CT, USA; Kent H. Casleton, Daniel J. Maloney, U.S. Department of Energy, Morgantown, WV, USA    2000-GT-0097 
IGTI  2000  NOx Scaling Characteristics for Industrial Gas Turbine Fuel Injectors  Donald W. Kendrick, Anuj Bhargava, Meredith B. Colket, William A. Sowa, United Technologies Research Center, East Hartford, CT, USA; Daniel J. Maloney, Kent H. Casleton, Department of Energy, Morgantown, WV, USA    2000-GT-0098 
IGTI  2000  Flamelet Model of NOx in a Diffusion Flame Combustor  Dmitry V. Volkov, Alexandr A. Belokon, Dmitry A. Lyubimov, Vladmir M. Zakharov, R&D Center ECOLEN, Moscow, Russia; George Opdyke, Jr., Power Tech Associates, Media, PA    2000-GT-0099 
IGTI  2000  Low-Emissions Gas Turbine Combustor Development for Regional-Class Aircraft  J. Zelina, Honeywell Engines and Systems, Phoenix, AZ, USA; P.F. Penko, NASA Glenn Research Center, Cleveland, OH, USA    2000-GT-0100 
IGTI  2000  Rapid Non-Intrusive Gas Turbine Exhaust Temperature Measurement  Michael A. Welch, Moira Hilton, University of Reading, Reading, UK; Chris W. Wilson, DERA Pyestock, Farnborough, UK    2000-GT-0101 
IGTI  2000  Closed-Loop Combustion Control Using OH Radical Emissions  Zhu (Julie) Meng, Robert J. Hoffa, Rolls-Royce Allison, Indianapolis, IN, USA; Charles A. DeMilo, Todd T. Thamer, AMETEK Power & Industrial Products, Wilmington, MA, USA    2000-GT-0102 
IGTI  2000  Ignition Delay Time Modulation as a Contribution to Thermo-Acoustic Instability in a Sequential Combustion  Alexander Ni, ABB Alstom Technology Ltd., Baden-Dättwil, Switzerland; Wolfgang Polifke, Technical University of Munich, Garching, Germany; Franz Joos, Fachhochschule Köln, Köln, Germany    2000-GT-0103 
IGTI  2000  Computational Modelling of Self-Excited Combustion Instabilities  Steve J. Brookes, R. Stewart Cant, Iain D.J. Dupere, Ann P. Dowling, University of Cambridge, Cambridge, UK    2000-GT-0104 
IGTI  2000  Prediction of Acoustic Pressure Spectra in Combustion Systems Using Swirl Stabilized Gas Turbine Burners  Bruno B.H. Schuermans, Christian Oliver Paschereit, Jan H. van der Linden, ABB Alstom Technology Center, Baden-Dättwil, Switzerland; Wolfgang Polifke, Technische Universität München, Munich, Germany    2000-GT-0105 
IGTI  2000  The Propagation of a Fuel-Air Ratio Disturbance in a Simple Premixer and its Influence on Pressure Wave Amplification  Thomas Scarinci, Rolls-Royce Canada Inc, Quebec, Canada; Christopher Freeman, Rolls-Royce plc, Derby, UK    2000-GT-0106 
IGTI  2000  Active Control Analysis for Combustion-Driven Dynamic Instabilities in Gas-Turbine Combustors  M.A. Mawid, T.W. Park, Engineering Research and Analysis Company, Dayton, OH, USA; B. Sekar, Air Force Research Laboratory, Wright-Patterson AFB, OH, USA    2000-GT-0107 
IGTI  2000  Self-excited Oscillations in Combustors with Spray Atomisers  M. Zhu, A.P. Dowling, K.N.C. Bray, University of Cambridge, Cambridge, UK    2000-GT-0108 
IGTI  2000  Industrial RB211 DLE Gas Turbine Combustion Update  Jeffrey D. Willis, A. John Moran, Rolls-Royce plc, Coventry, UK    2000-GT-0109 
IGTI  2000  Experimental and Theoretical Studies of a Novel Venturi LPP Combustor  Nils A. Røkke, Andrew J.W. Wilson, Ulstein Turbine AS, Bergen, Norway    2000-GT-0110 
IGTI  2000  Dual Fuel Dry Low Emissions (DLE) Combustion System for the ABB Alstom Power 13,4 MW Cyclone Gas Turbine  H. Alkabie, R. McMillan, R. Noden, C. Morris, ABB Alstom Power UK Ltd., Lincoln, UK    2000-GT-0111 
IGTI  2000  Dual Fuel DLE Typhoon Commercial Operating Experience and Improvement Upgrades  P. Taylor, The Boots Company PLC, Nottingham, UK; R. McMillan, D. Baker, ABB Alstom Power, Lincoln, UK    2000-GT-0112 
IGTI  2000  Research on a Methane-Fueled Low NOx Combustor for a Mach 3 Supersonic Transporter Turbojet Engine  Yasuhiro Kinoshita, Takeo Oda, Junichi Kitajima, Kawasaki Heavy Industries, Ltd., Akashi, Japan    2000-GT-0113 
IGTI  2000  Improvement of Aerodynamic Performance of a Combustor Dump Diffuser Using Inclined Walls  Shinji Honami, Takaaki Shizawa, The Science University of Tokyo, Tokyo, Japan; Eiichi Yamazaki, Fukushima Nuclear Power Plant, Fukushima, Japan    2000-GT-0114 
IGTI  2000  Application of Macrolamination Technology to Lean, Premix Combustion  Adel Mansour, Michael Benjamin, Parker Hannifin Corporation, Mentor, OH, USA; Douglas L. Straub, Geo. A. Richards, U.S. Department of Energy, Morgantown, WV, USA    2000-GT-0115 
IGTI  2000  Rapid Liquid Fuel Mixing for Lean-Burning Combustors: Low-Power Performance  May Y. Leong, Craig S. Smugeresky, Vincent G. McDonell, G. Scott Samuelsen, University of California, Irvine, CA, USA    2000-GT-0116 
IGTI  2000  A New Hybrid Air Blast Nozzle for Advanced Gas Turbine Combustors  Adel Mansour, Michael Benjamin, Erlendur Steinthorsson, Parker Hannifin Corporation, Mentor, OH, USA    2000-GT-0117 
IGTI  2000  Flow and Spray Characteristics of a Lean Fuel Injection Module with Radial Swirlers  Woo Seok Seol, Yeoung Min Han, Dae Sung Lee, Korea Aerospace Research Institute, Taejon, Korea    2000-GT-0118 
IGTI  2000  Internal Flow Structure of a Pressure-Swirl Atomizer at Two Different Density Ratios  Dexin Wang, Zhanhua Ma, San-Mou Jeng, University of Cincinnati, Cincinnati, OH, USA; Michael A. Benjamin, Parker Hannifin Corporation, Mentor, OH, USA    2000-GT-0119 
IGTI  2000  Flow Structures of a Radial-Inlet Swirler  Zhanhua Ma, Dexin Wang, San-Mou Jeng, University of Cincinnati, Cincinnati, OH, USA; Michael A. Benjamin, Parker Hannifin Corporation, Mentor, OH, USA    2000-GT-0120 
IGTI  2000  An Examination of the Relationship Between Chemiluminescent Light Emissions and Heat Release Rate Under Non-Adiabatic Conditions  Ludwig C. Haber, Uri Vandsburger, William R. Saunders, Vivek K. Khanna, Virgina Tech, Blacksburg, VA, USA    2000-GT-0121 
IGTI  2000  Integrated Experimental and Numerical Approach for Fuel-Air Mixing Prediction in a Heavy-Duty Gas Turbine LP Burner  Giulo Mori, Sandro Razore, Ansaldo Ricerche s.r.l., Genova, Italy; Marina Ubaldi, Pietro Zunino, Università di Genova, Genova, Italy    2000-GT-0122 
IGTI  2000  Experimental and Numerical Investigation of a Planar Combustor Sector at Realistic Operating Conditions  Thomas Behrendt, Martin Carl, Christian Fleing, Matthias Frodermann, Johannes Heinze, Christoph Hassa, German Aerospace Center, Cologne, Germany; Ulrich Meier, Dagmar Wolff-Gaßmann, German Aerospace Center, Stuttgart, Germany; Stefan Hohmann, Nikolaos Zar    2000-GT-0123 
IGTI  2000  Feasibility Studies and Application of Laser/Optical Diagnostics for Characterisation of a Practical Low-Emission Gas Turbine Combustor  C. Löfström, J. Engström, M. Richter, C.F. Kaminski, K. Nyholm, J. Hult, J. Nygren, M. Aldén, Lund Institute of Technology, Lund, Sweden; P. Johansson, Volvo Aero Corporation, Trollhättan, Sweden    2000-GT-0124 
IGTI  2000  Coupled and Uncoupled CFD Prediction of the Characteristics of Jets from Combustor Air Admission Ports  J.J. McGuirk, A. Spencer, Loughborough University, Loughborough, Leicestershire, UK    2000-GT-0125 
IGTI  2000  Design of a Jet-Stirred Gas Generator for Studies of High Temperature Mixing and Combustion  C.G. Fotache, D.J. Hautman, T.J. Rosfjord, United Technologies Research Center, East Hartford, CT, USA    2000-GT-0127 
IGTI  2000  An Accurate and Affordable Spray Model for Gas Turbine Combustor Design  Anil K. Tolpadi, General Electric Research & Development Center, Schenectady, NY, USA; Suresh K. Aggarwal, University of Illinois at Chicago, Chicago, IL, USA; Hukam C. Mongia, General Electric Aircraft Engines, Cincinnati, OH, USA    2000-GT-0128 
IGTI  2000  Parametric Modeling Approach to Gas Turbine Combustor Design  Venkat E. Tangirala, Anil K. Tolpadi, General Electric Research & Development Center, Schenectady, NY, USA; Al M. Danis, Hukam Mongia, General Electric Aircraft Engines, Cincinnati, OH, USA    2000-GT-0129 
IGTI  2000  Modelling of the Combustion Process of a Premixed DLE Gas Turbine  R.L.G.M. Eggels, Rolls Royce plc, Coventry, UK    2000-GT-0130 
IGTI  2000  CFD Analysis of a Complete Industrial Lean Premixed Gas Turbine Combustor  P. Birkby, R.S. Cant, W.N. Dawes, A.A.J. Demargne, P.C. Dhanasekaran, W.P. Kellar, N.C. Rycroft, A.M. Savill, University of Cambridge, Cambridge, UK; R.L.G.M. Eggels, I.K. Jennions, Rolls-Royce plc, Coventry, UK    2000-GT-0131 
IGTI  2000  Evaluation of Advanced Two-Phase Flow and Combustion Models for Predicting Low Emission Combustors  G. Klose, R. Schmehl, R. Meier, G. Meier, R. Koch, S. Wittig, M. Hettel, W. Leuckel, Universität Karlsruhe, Karlsruhe, Germany; N. Zarzalis, DaimlerChrysler Aerospace, München, Germany    2000-GT-0133 
IGTI  2000  The Structure of Two-Stage Counterflow n-Heptane-Air Flames  S.K. Aggarwal, H.S. Xue, University of Illinois at Chicago, Chicago, IL, USA    2000-GT-0134 
IGTI  2000  Modeling of Inhomogeneously Premixed Combustion with an Extended TFC Model  Wolfgang Polifke, Technical University of Munich, Garching, Germany; Peter Flohr, ABB Alstom Power Technology Ltd., Baden, Switzerland; Martin Brandt, Fachhochschule Karlsruhe, Karlsruhe, Germany    2000-GT-0135 
IGTI  2000  Experimental and Numerical Investigation on the Evaporation of Shear-Driven Multi-Component Liquid Wall Films  M. Gerendas, S. Wittig, Universität Karlsruhe, Karlsruhe, Germany    2000-GT-0136 
IGTI  2000  Use of Chromium Containing Fuel Additive to Reduce High Temperature Corrosion of Hot Section Parts  Jean-Pierre Stalder, Peter A. Huber, Turbotect Ltd., Baden, Switzerland    2000-GT-0138 
IGTI  2000  Alternative Fuels in Gas Turbine Applications: A Simple Method for Assessing the Influence of Fuel on Performances  Michel Molière, Frédéric Pommel, General Electric Energy Products - Europe, Belfort, France    2000-GT-0139 
IGTI  2000  Response of a Model Gas Turbine Combustor to Variation in Gaseous Fuel Composition  R.M. Flores, M.M. Miyasato, V.G. McDonnell, G.S. Samuelsen, University of California, Irvine, CA, USA    2000-GT-0141 
IGTI  2000  Implementation and Validation of a New Soot Model and Application to Aeroengine Combustors  M. Balthasar, F. Mauss, Lund Institute of Technology, Lund, Sweden; M. Pfitzner, A. Mack, BMW Rolls-Royce AeroEngines, Dahlewitz, Germany    2000-GT-0142 
IGTI  2000  Numerical Simulation of Swirl-Stabilized Premixed Flames with a Turbulent Combustion Model Based on a Systematically Reduced 6-Step Reaction Mechanism  Dieter E. Bohn, Joachim Lepers, Aachen University of Technology, Aachen, Germany    2000-GT-0143 
IGTI  2000  Flamelet Studies of Reduced and Detailed Kinetic Mechanisms for Methane/Air Diffusion Flames  Foluso Ladeinde, SUNY, Stony Brook, NY, USA; Xiaodan Cai, Aerospace Research Corp., L.I., Stony Brook, NY, USA; Balu Sekar, Air Force Research Laboratory, Wright-Patterson AFB, OH, USA    2000-GT-0144 
IGTI  2000  Reaction Mechanisms for Methane Ignition  S.C. Li, F.A. Williams, University of California, San Diego, La Jolla, CA, USA    2000-GT-0145 
IGTI  2000  Computation of 3D Turbulent Not-premixed Reacting Flows Using an Implicit Unstructured Solver  P. Adami, F. Martelli, University of Florence, Florence, Italy    2000-GT-0147 
IGTI  2000  Control Optimization of the Transient Performance of the Selective Bleed Variable Cycle Engine During Mode Transition  U.T.J. Grönstedt, Chalmers University of Technology, Gothenburg, Sweden; P. Pilidis, Cranfield University, Cranfield, Bedford, UK    2000-GT-0148 
IGTI  2000  An Approximate Method for Jet Engines Flight Performances Prediction  A. Ghenaiet, Thermal Power Laboratory, Bordj El Bahri, Algeria    2000-GT-0149 
IGTI  2000  Introduction of Intercooling in a High Bypass Jet Engine  Tilemachos Papadopoulos, Pericles Pilidis, Cranfield University, Cranfield, Bedfordshire, UK    2000-GT-0150 
IGTI  2000  Assessment of Remote Lift Fan Jet Engines  Luca Arnulfo, Pericles Pilidis, Cranfield University, Cranfield, Bedford, UK    2000-GT-0151 
IGTI  2000  Gas Turbine Performance Using Carbon Dioxide as Working Fluid in Closed Cycle Operation  Anthony J.B. Jackson, Alcides Codeceira Neto, Matthew W. Whellens, Cranfield University, Cranfield, UK; Harry Audus, IEA Greenhouse Gas R&D Programme, Cheltenham, UK    2000-GT-0153 
IGTI  2000  Semi-Closed HAT (SC-HAT) Power Cycle  Carlo Carcasci, Lorenzo Cosi, Daniele Fiaschi, Giampaolo Manfrida, Università degli Studi di Firenze, Firenze, Italia    2000-GT-0154 
IGTI  2000  On-Design and Off-Design Performance Analysis of a Gas Turbine Combined Cycle Using the Exergy Method  Alcides Codeceira Neto, Pericles Pilidis, Cranfield University, Cranfield, UK    2000-GT-0155 
IGTI  2000  Thermodynamic Optimization of Reheat Gas Turbine Cycles Combined with Bottoming Cycles  Isaac Shnaid, The Israel Electric Corporation Ltd., Haifa, Israel    2000-GT-0156 
IGTI  2000  Repowering of an Existing Cogeneration Plant Including Environmental Cost Internalization  M. Cali, M. Santarelli, Politecnico di Torino, Torino, Italy; A.F. Massardo, Università di Genova, Genova, Italy    2000-GT-0157 
IGTI  2000  Design Study of Helium Turbine for the 300MW HTGR-GT Power Plant  Yasushi Muto, Shintaro Ishiyama, Japan Atomic Energy Research Institute, Oarai Ibaraki, Japan; Yoshitako Fukuyama, Junji Okumoto, Toshiba Corporation, Yokohama, Japan; Tadaharu Kishibe, Hitachi, Ltd., Hitachinaka, Japan; Seiya Yamada, Mitsubishi Heavy Ind    2000-GT-0159 
IGTI  2000  New Concept of CO2 Removal Technologies in Power Generation Combined with Fossil Fuel Recovery and Long Term CO2 Sequestration  Ph. Mathieu, R. Dubuisson, S. Houyou, R. Nihart, University of Liège, Liège, Belgium    2000-GT-0160 
IGTI  2000  Performance Assessment of Semi-Closed Chemically Recuperated Gas Turbine Systems  Giorgio Cau, Daniele Cocco, University of Cagliari, Cagliari, Italy    2000-GT-0161 
IGTI  2000  Gas Turbine Combined Cycle with CO2-Capture Using Auto-Thermal Reforming of Natural Gas  Thormod Andersen, Hanne M. Kvamsdal, SINTEF Energy Research, Trondheim, Norway; Olav Bolland, The Norweigian University of Science and Technology, Trondheim, Norway    2000-GT-0162 
IGTI  2000  Natural Gas Decarbonization to Reduce CO2 Emission from Combined Cycles. Part A: Partial Oxidation  Giovanni Lozza, Paolo Chiesa, Politecnico di Milano, Milan, Italy    2000-GT-0163 
IGTI  2000  Natural Gas Decarbonization to Reduce CO2 Emission from Combined Cycles. Part B: Steam-Methane Reforming  Giovanni Lozza, Paolo Chiesa, Politecnico di Milano, Milan, Italy    2000-GT-0164 
IGTI  2000  Assessment of LNG Regasification Systems with Cogeneration  Umberto Desideri, Claudio Belli, Università di Perugia, Perugia, Italy    2000-GT-0165 
IGTI  2000  An Ericsson Cycle GT Design by LNG Cryogenic Heat Utilization  Kirk Hanawa, Ishikawajima Harima Heavy Industries, Co., Ltd., Tokyo, Japan    2000-GT-0166 
IGTI  2000  Low Cost Recuperator Concept for Microturbine Applications  Colin F. McDonald, McDonald Thermal Engineering, LaJolla, CA, USA    2000-GT-0167 
IGTI  2000  First Experiments on an Evaporative Gas Turbine Pilot Power Plant - Water Circuit Chemistry and Humidification Evaluation  Niklas D. Ågren, Mats O. Westermark, Michael A. Bartlett, Royal Institute of Technology, Stockholm, Sweden; Torbjörn Lindquist, Lund Institute of Technology, Lund, Sweden    2000-GT-0168 
IGTI  2000  Comparison of Gas Turbine Cooling with Dry Air, Humidified Air and Steam  Kristin Jordal, Tord Torisson, Lund Institute of Technology, Lund, Sweden    2000-GT-0169 
IGTI  2000  Dynamic Modelling of the Gasification Island of a Coal-Based IGCC  Raoul Nihart, University of Liège, Liège, Belgium    2000-GT-0170 
IGTI  2000  Aero-Thermodynamic Simulation of a Double-Shaft Industrial Evaporative Gas Turbine  S.M. Camporeale, University of Reggio Calabria, Reggio Calabria, Italy; B. Fortunato, Polytechnic University of Bari, Bari, Italy    2000-GT-0171 
IGTI  2000  Conceptual Design for Medium Size Combined Cycle Plants Improved by Recent Research and Innovation  H. Jericha, F. Neumayer, Technical University of Graz, Graz, Austria    2000-GT-0172 
IGTI  2000  Estimation of the Operating Characteristics of the Adjustable Speed Gas Turbine Power Generation System During Partial Load Operation  Naoyuki Nagafuchi, Nariyoshi Kobayashi, Hitachi Ltd., Hitachinaka-shi, Japan; Motoaki Utamura, Hitachi, Ltd., Hitachi-shi, Japan    2000-GT-0173 
IGTI  2000  Assessment of Molten Carbonate Fuel Cell Models and Integration with Gas and Steam Cycles  A.F. Massardo, B. Bosio, Università di Genova, Genova, Italy    2000-GT-0174 
IGTI  2000  Microturbine/Fuel-Cell Coupling for High-Efficiency Electrical-Power Generation  Aristide F. Massardo, Università di Genova, Genova, Italy; Colin F. McDonald, McDonald Thermal Engineering, La Jolla, CA, USA; Theodosios Korakianitis, Washington University, St. Louis, MO, USA    2000-GT-0175 
IGTI  2000  Developing the Next Generation Gas Turbine Systems - A National Partnership  A.W. Layne, U.S. Department of Energy, Morgantown, WV, USA    2000-GT-0176 
IGTI  2000  Managing Fuel Oil Nozzle Coking to Improve Gas Turbine Availability  Leo R. Burgett, ABB Alstom Power Inc., Midlothian, VA, USA; Tim Mercer, Savannah Electric & Power Company, Rincon, GA, USA    2000-GT-0177 
IGTI  2000  Hot-Gas-Path Life Extension Options for the V94.2 Gas Turbine  Gerhard Bohrenkämper, Herbert Bals, Ursel Wrede, Siemens AG, Power Generation KWU, Mülheim a.d. Ruhr, Germany; René Umlauft, Siemens AG, Power Generation KWU, Berlin, Germany    2000-GT-0178 
IGTI  2000  Early Detection of Combustor Pulsations and Optimized Operation Through On-Line Monitoring Systems  Helmer Andersen, ABB ALSTOM Power, Midlothian, VA, USA    2000-GT-0180 
IGTI  2000  Power Plants Up-Rating Benefit from Technology Advancements  Robert McCue, Midland Cogneration Venture, Midlan, MI, USA; Axel W. von Rappard, ABB Alstom Power, Surprise, AZ, USA    2000-GT-0181 
IGTI  2000  Integration of a Gas Turbine (GT) with a Compressed Air Storage (CAES) Plant Provides the Best Alternative for Mid-Range and Daily Cyclic Generation Needs  Michael Nakhamkin, Energy Storage and Power Consultants, Inc., Mountainside, NJ, USA; Septimus van der Linden, ABB ALSTOM Power, Midlothian, VA, USA    2000-GT-0182 
IGTI  2000  Life Extension of GT HGP Components by Recycling  Jung-Ho Lee, P.C. Engineering Company, Seoul, Korea    2000-GT-0184 
IGTI  2000  A Neural Network Simulator of a Gas Turbine with a Waste Heat Recovery Section  C. Boccaletti, G. Cerri, B. Seyedan, University ROMA TRE, Roma, Italy    2000-GT-0185 
IGTI  2000  Manufacturers' Role in the Power Industry  Dilip K. Mukherjee, ABB ALSTOM POWER, Baden, Swizterland    2000-GT-0186 
IGTI  2000  Development of a Maintenance Program for Major Gas Turbine Hot Gas Path Parts  Hideto Moritsuka, Tomoharu Fujii, Takeshi Takahashi, Central Research Institute of Electric Power Industry, Yokosuka-City, Kanagawa-Pref, Japan    2000-GT-0187 
IGTI  2000  Risk-Based Inspection of Combustion Turbines  Michael E.G. Schmidt, Industrial Risk Insurers, Hartford, CT, USA; David A. Mauney, Structural Integrity Associates, Inc., Rockville, MD, USA    2000-GT-0189 
IGTI  2000  World's First LM5000 to LM6000 Cogeneration Plant Repowering  Michael T. McCarrick, Robert K. Rosencrance, Energy Services, Inc., Farmington, CT, USA    2000-GT-0190 
IGTI  2000  Combustion Turbine Inlet Conditioning - A State-of-the-Art Method of Increasing Generating Capacity Without the Addition of New Basic Generation Hardware  Lloyd B. Tisdale, Tisdale Company, Incorporated, Conroe, TX, USA; Robert L. Hauck, HouRep, Incorporated, Houston, TX, USA    2000-GT-0192 
IGTI  2000  Leakage Flow Over Shrouded Turbine Blades  Yumin Xiao, R.S. Amano, University of Wisconsin-Milwaukee, Milwaukee, WI, USA    2000-GT-0193 
IGTI  2000  Heat Transfer and Pressure Distributions on a Gas Turbine Blade Tip  Gm S. Azad, Je-Chin Han, Shuye Teng, Texas A&M University, College Station, TX, USA; Robert J. Boyle, NASA Glenn Research Center, Cleveland, OH, USA    2000-GT-0194 
IGTI  2000  Heat Transfer and Flow on Squealer Tip of a Gas Turbine Blade  Gm S. Azad, Je-Chin Han, Texas A&M University, College Station, TX, USA; Robert J. Boyle, NASA Glenn Research Center, Cleveland, OH, USA    2000-GT-0195 
IGTI  2000  Experimental Investigations on the Thermal Load and Leakage Flow of a Turbine Blade Tip Section with Different Tip Section Geometries  Martin F. Urban, Nicolas Vortmeyer, Siemens AG, KWU Group, Muelheim, Germany    2000-GT-0196 
IGTI  2000  Time-Averaged Heat Flux for a Recessed Tip, Lip, and Platform of a Transonic Turbine Blade  M.G. Dunn, C.W. Haldeman, The Ohio State University Gas Turbine Laboratory, Columbus, OH, USA    2000-GT-0197 
IGTI  2000  Flow and Heat Transfer at the Hub Endwall of Inlet Vane Passages: Experiments and Simulations  R.P. Roy, K.D. Squires, M. Gerendas, S. Song, Arizona State University, Tempe, AZ, USA; W.J. Howe, A. Ansari, AlliedSignal Engines, Phoenix, AZ, USA    2000-GT-0198 
IGTI  2000  Effects of Slot Bleed Injection Over a Contoured Endwall on Nozzle Guide Vane Cooling Performance: Part I -Flow Field Measurements  Steven W. Burd, Pratt & Whitney, East Hartford, CT, USA; Terrence W. Simon, University of Minnesota, Minneapolis, MN, USA    2000-GT-0199 
IGTI  2000  Effects of Slot Bleed Injection Over a Contoured End Wall on Nozzle Guide Vane Cooling Performance: Part II - Thermal Measurements  Steven W. Burd, Pratt & Whitney, East Hartford, CT, USA; Cynthia J. Satterness, Terrence W. Simon, University of Minnesota, Minneapolis, MN, USA    2000-GT-0200 
IGTI  2000  High Freestream Turbulence Effects on Endwall Heat Transfer for a Gas Turbine Stator Vane  R.W. Radomsky, K.A. Thole, Virginia Polytechnic Institute and State University, Blacksburg, VA, USA    2000-GT-0201 
IGTI  2000  Investigation of Heat Transfer in a Film Cooled Transonic Turbine Cascade, Part II: Unsteady Heat Transfer  O. Popp, D.E. Smith, J.V. Bubb, H.C. Grabowski III, T.E. Diller, J.A. Schetz, W.F. Ng, Virginia, Polytechnic Institute and State University, Blacksburg, VA, USA    2000-GT-0202 
IGTI  2000  Investigation of Heat Transfer in a Film Cooled Transonic Turbine Cascade, Part I: Steady Heat Transfer  D.E. Smith, J.V. Bubb, O. Popp, H. Grabowski III, T.E. Diller, J.A. Schetz, W.F. Ng, Virginia Polytechnic Institute and State University, Blacksburg, VA, USA    2000-GT-0203 
IGTI  2000  Influence Of Surface Roughness on Heat Transfer and Effectiveness for a Fully Film Cooled Nozzle Guide Vane Measured by Wide Band Liquid Crystals and Direct Heat Flux Gauges  S.M. Guo, C.C. Lai, T.V. Jones, M.L.G. Oldfield, University of Oxford, England, UK; G.D. Lock, University of Bath, Bath, England, UK; A.J. Rawlinson, Rolls-Royce plc, Derby, England, UK    2000-GT-0204 
IGTI  2000  The Influence of the Boundary Layer State and Reynolds Number on Film Cooling and Heat Transfer on a Cooled Nozzle Guide Vane  Hans Reiss, Albin Bölcs, Swiss Federal Institute of Technology, Lausanne, Switzerland    2000-GT-0205 
IGTI  2000  Influence of Vane/Blade Spacing on the Heat Flux for a Transonic Turbine  M.G. Dunn, C.W. Haldeman, R.S. Abhari, M.L. McMillan, The Ohio State University, Columbus, OH, USA    2000-GT-0206 
IGTI  2000  Cooling Effectiveness Measurements with Thermal Radiometry in a Turbine Cascade  H.K. Moon, R. Jaiswal, Solar Turbines Incorporated, San Diego, CA, USA    2000-GT-0207 
IGTI  2000  Rotor/Stator Heat Transfer Measurements and CFD Predictions for Short-Duration Turbine Rig Tests  Robert F. Bergholz, Gary D. Steuber, GE Aircraft Engines, Cincinnati, OH, USA; Michael G. Dunn, Ohio State University, Columbus, OH, USA    2000-GT-0208 
IGTI  2000  Heat Transfer Measurements and Predictions on a Power Generation Gas Turbine Blade  Paul W. Giel, Dynacs Engineering Co., Inc., Brook Park, OH, USA; Ronald S. Bunker, General Electric Corporation, Schenectady, NY, USA; G. James Van Fossen, Robert J. Boyle, NASA Glenn Research Center, Cleveland, OH, USA    2000-GT-0209 
IGTI  2000  Aerodynamics and Heat Transfer in a Turbine Blade at Design and Off-Design Angles of Incidence  C. Xu, R.S. Amano, University of Wisconsin-Miwaukee, Milwaukee, WI, USA    2000-GT-0210 
IGTI  2000  Analysis of Flow and Heat Transfer in the End-Wall Region of a Turbine Blade Passage  Yumin Xiao, R.S. Amano, University of Wisconsin-Milwaukee, Milwaukee, WI, USA    2000-GT-0211 
IGTI  2000  Secondary Flow Measurements in a Turbine Passage with Endwall Flow Modification  Nicole V. Aunapu, Ralph J. Volino, Karen A. Flack, Ryan M. Stoddard, United States Naval Academy, Annapolis, MD, USA    2000-GT-0212 
IGTI  2000  Flow Measurements in a Nozzle Guide Vane Passage with a Low Aspect Ratio and Endwall Contouring  Steven W. Burd, Pratt and Whitney, East Hartford, CT, USA; Terrence W. Simon, University of Minnesota, Minneapolis, MN, USA    2000-GT-0213 
IGTI  2000  Measurements in a Turbine Cascade Over a Contoured Endwall: Discrete Hole Injection of Bleed Flow  Rohit A. Oke, Terrence W. Simon, University of Minnesota, Minneapolis, MN, USA; Steven W. Burd, Pratt and Whitney, East Hartford, CT, USA; Rickard Vahlberg, Royal Swedish Institute, Stockholm, Sweden    2000-GT-0214 
IGTI  2000  Augmentation of Stagnation Region Heat Transfer Due to Turbulence from a DLN Can Combustor  G. James Van Fossen, NASA Glenn Research Center, Cleveland, OH, USA; Ronald S. Bunker, General Electric, Schenectady, NY, USA    2000-GT-0215 
IGTI  2000  Infared Low Temperature Turbine Vane Rough Surface Heat Transfer Measurements  R.J. Boyle, B.L. Lucci, C.M. Spuckler, W.P. Camperchioli, NASA Glenn Research Center, Cleveland, OH, USA    2000-GT-0216 
IGTI  2000  Comparison of Predicted and Measured Turbine Vane Rough Surface Heat Transfer  R.J. Boyle, B.L. Lucci, C.M. Spuckler, NASA Glenn Research Center, Cleveland, OH, USA    2000-GT-0217 
IGTI  2000  The Two-Flux Model Applied to Radiative Transfer and Forced Convection in the Laminar Boundary Layer on a Flat Plate  Freddy Malpica, Nathaly Moreno, Andrés Tremante, Universidad Simón Bolívar, Caracas, Venezuela    2000-GT-0218 
IGTI  2000  Heat Transfer and Flow Characteristics of an Engine Representative Impingement Cooling System  Changmin Son, David Gillespie, Peter Ireland, University of Oxford, Oxford, UK; Geoffrey M. Dailey, Rolls-Royce plc, Derby, UK    2000-GT-0219 
IGTI  2000  Experimental Investigation on Impingement Heat Transfer from Rib Roughened Surface Within Arrays of Circular Jets: Correlation  Chang Hiaping, Zhang Jingyu, Nanjing University of Aeronautics and Astronautics, Nanjing, China; Huang Taiping, Xiamen University, Xiamen, China    2000-GT-0220 
IGTI  2000  Mist/Steam Heat Transfer in Confined Slot Jet Impingement  X. Li, J.L. Gaddis, Clemson University, Clemson, SC, USA; T. Wang, University of New Orleans, New Orleans, LA, USA    2000-GT-0221 
IGTI  2000  An Experimental Evaluation of Advanced Leading Edge Impingement Cooling Concepts  M.E. Taslim, L. Setayeshgar, Northeastern University, Boston, MA, USA; S.D. Spring, GE Aircraft Engines, Lynn, MA, USA    2000-GT-0222 
IGTI  2000  Flow and Heat Transfer of Confined Impingement Jets Cooling  Ting Wang, University of New Orleans, New Orleans, LA, USA; Mingjie Lin, Clemson University, Clemson, SC, USA; Ronald S. Bunker, General Electric Corporate R&D, Schenectady, NY, USA    2000-GT-0223 
IGTI  2000  Heat Transfer in Rotating Narrow Rectangular Ducts with Heated Sides Oriented at 60° to the R-Z Plane  Fred T. Willett, Authur E. Bergles, Rensselaer Polytechnic Institute, Troy, NY, USA    2000-GT-0224 
IGTI  2000  Application of Non-Linear k-w Model to the Turbulent Flow inside a Sharp U-Bend  B. Song, R.S. Amano, University of Wisconsin-Milwaukee, Milwaukee, MI, USA    2000-GT-0225 
IGTI  2000  Heat Transfer Enhancements in Rotating Two-Pass Coolant Channels with Profiled Ribs: Part 2 - Detailed Measurements  D.E. Nikitopoulos, V. Eliades, S. Acharya, Louisiana State University, Baton Rouge, LA, USA    2000-GT-0226 
IGTI  2000  Heat Transfer Enhancements in Rotating Two-Pass Coolant Channels with Profiled Ribs: Part 1 - Average Results  S. Acharya, V. Eliades, D.E. Nikitopoulos, Louisiana State University, Baton Rouge, LA, USA    2000-GT-0227 
IGTI  2000  Rotating Effect on Fluid Flow in a Smooth Duct with 180-Deg Sharp Turn  Chung-Chu Chen, Tong-Min Liou, National Tsing Hua University, Hsinchu, Taiwan    2000-GT-0228 
IGTI  2000  Flow and Heat Transfer in a Rotating Square Channel with 45º Angled Ribs by Reynolds Stress Turbulence Model  Yong-Jun Jang, Hamn-Ching Chen, Je-Chin Han, Texas A&M University, College Station, TX, USA    2000-GT-0229 
IGTI  2000  Local Heat Transfer and Flow Structure on and Above a Dimpled Surface in a Channel  G.I. Mahmood, M.L. Hill, D.L. Nelson, P.M. Ligrani, University of Utah, Salt Lake City, UT, USA; H-K. Moon, B. Glezer, Solar Turbines, Inc., San Diego, CA, USA    2000-GT-0230 
IGTI  2000  A Transient Liquid Crystal Method Using Hue Angle and a 3-D Inverse Transient Conduction Scheme  Mingjie Lin, Clemson University, Clemson, SC, USA; Ting Wang, University of New Orleans, LA, USA    2000-GT-0231 
IGTI  2000  Lateral-Flow Effect on Endwall Heat Transfer and Pressure Drop in a Pin-Fin Trapezoidal Duct of Various Pin Shapes  Jenn-Jiang Hwang, Chau-Ching Lu, Chung-Hua University, Hsinchu, Taiwan    2000-GT-0232 
IGTI  2000  Experimental Heat Transfer and Bulk Air Temperature Measurements for Multipass Internal Cooling Model with Ribs and Bleed  Douglas Thurman, Philip Poinsatte, Glenn Research Center, Cleveland, OH, USA    2000-GT-0233 
IGTI  2000  Intercoolers in Gas Turbine Systems and Combi-Processes for Production of Electricity  Arash Saidi, Bengt Sundén, Daniel Eriksson, Lund Institute of Technology, Lund, Sweden    2000-GT-0234 
IGTI  2000  Influence of Cross-Flow Induced Swirl and Impingement on Heat Transfer in a Two-Pass Channel Connected by Two Rows of Holes  Gautam Pamula, Srinath V. Ekkad, Sumanta Acharya, Louisiana State University, Baton Rouge, LA, USA    2000-GT-0235 
IGTI  2000  Effect of Surface Curvature on Heat Transfer and Hydrodynamics Within a Single Hemispherical Dimple  N. Syred, A. Khalatov, Cardiff University, Cardiff, UK; A. Kozlov, Russian Academy of Sciences, City of Kazan, Russia; A. Shchukin, R. Agachev, Kazan State Technical University, City of Kazan, Russia    2000-GT-0236 
IGTI  2000  Innovative Cyclone Cooling Scheme for Gas Turbine Blade: Thermal-Hydraulic Performance Evaluation  Artem Khalatov, Nick Syred, Philip Bowen, Rashed Al-Ajmi, Cardiff University, Cardiff, UK; Alexander Kozlov, Russian Academy of Sciences, City of Kazan, Russia; Andrey Schukin, Kazan State Technical University (KAI), City of Kazan, Russia    2000-GT-0237 
IGTI  2000  Influence of Injection Type and Feed Arrangement on Flow and Heat Transfer in an Injection Slot  Hyung Hee Cho, Yonsei University, Seoul, Korea; Jin Ki Ham, Hyundai Heavy Industries Co., Ltd., Ulsan, Korea    2000-GT-0238 
IGTI  2000  Scaling of Performance for Varying Density Ratio Coolants on an Airfoil with Strong Curvature and Pressure Gradient Effects  Marcia I. Ethridge, J. Michael Cutbirth, David G. Bogard, The University of Texas at Austin, Austin, TX, USA    2000-GT-0239 
IGTI  2000  Effects of Showerhead Injection on Film Cooling Effectiveness for a Downstream Row of Holes  Marc D. Polanka, Marcia I. Ethridge, J. Michael Cutbirth, David G. Bogard, The University of Texas at Austin, Austin, TX, USA    2000-GT-0240 
IGTI  2000  Novel Blade Cooling Engineering Solution  Siegfried Moser, Mario Ivanisin, Jakob Woisetschläger, Herbert Jericha, Technical University Graz, Graz, Austria    2000-GT-0242 
IGTI  2000  Measurement of Local Heat Transfer Coefficient and Film Cooling Effectiveness Through Discrete Holes  R.F. Martinez-Botas, C.H.N. Yuen, Imperial College of Science, Technology, and Medicine, London, UK    2000-GT-0243 
IGTI  2000  Effect of Partial Coating Blockage on Film Cooling Effectiveness  Ronald S. Bunker, General Electric Corp. R&D Center, Schenectady, NY, USA    2000-GT-0244 
IGTI  2000  Transient Liquid Crystal Measurement of Leading Edge Film Cooling Effectiveness and Heat Transfer with High Free Stream Turbulence  Shichuan Ou, Richard Rivir, Matthew Meininger, Air Force Research Laboratory, WPAFB, OH, USA; Fred Soechting, Martin Tabbita, Pratt & Whitney Aircraft Engines, West Palm Beach, FL, USA    2000-GT-0245 
IGTI  2000  The Effects of Injection Angle and Hole Exit Shape on Turbine Nozzle Pressure Side Film Cooling  Luzeng J. Zhang, Ram Pudupatty, Solar Turbines Incorporated, San Diego, CA, USA    2000-GT-0247 
IGTI  2000  Film Cooling Downstream of a Row of Discrete Holes with Compound Angle  R.J. Goldstein, P. Jin, University of Minnesota, Minneapolis, MN, USA    2000-GT-0248 
IGTI  2000  Reynolds Stress Transport Model Predictions and Large Eddy Simulations for Film Coolant Jet in Crossflow  Asif Hoda, Acharya Sumanta, Mayank Tyagi, Louisiana State University, Baton Rouge, LA, USA    2000-GT-0249 
IGTI  2000  Numerical and Experimental Investigations of the Influence of Different Swirl Ratios on the Temperature Streak Development in a 4-Stage Turbine  Dieter Bohn, Harald Funke, Tom Heuer, Aachen University of Technology, Aachen, Germany; Jürg Bütikofer, ABB Alstom Power, Baden, Switzerland    2000-GT-0250 
IGTI  2000  Thermal Conjugate Analysis of a First Stage Blade in a Gas Turbine  Toshihiko Takahashi, Kazunori Watanabe, Takeshi Takahashi, Central Research Institute of Electric Power Industry, Yokosuka, Kanagawa, Japan    2000-GT-0251 
IGTI  2000  Local Heat/Mass Transfer Measurement on the Effusion Plate in Impingement/Effusion Cooling System  Hyung Hee Cho, Dong Ho Rhee, Yonsei University, Seoul, Korea    2000-GT-0252 
IGTI  2000  Simultaneous Prediction of External Flow-Field and Temperature in Internally Cooled 3-D Turbine Blade Material  Zhen-Xue Han, George S. Dulikravich, University of Texas at Arlington, Arlington, TX, USA; Brian H. Dennis, The Pennsylvania State University, University Park, PA, USA    2000-GT-0253 
IGTI  2000  Heat Transfer Analysis in a Modern DLN Combustor  Giovanni Ferrara, Luca Innocenti, Giacomo Migliorini, Università degli Studi di Firenze, Firenze,Italy; Bruno Facchini, Università degli Studi di Parma, Parma, Italy; Anthony J. Dean, GE Corporate Research and Development, Niskayuna, NY, USA    2000-GT-0254 
IGTI  2000  Turbulence Structures of Leading Edge Film Cooling Jets  Sabine Ardey, Motoren- und Turbinen-Union München GmbH, München, Germany; Stefan Wolff, Leonhard Fottner, Universität der Bundeswehr München, Neubiberg, Germany    2000-GT-0255 
IGTI  2000  Flow Characteristics Inside Circular Injection Holes Normally Oriented to a Crossflow: Part I - Flow Visualizations and Flow Data in the Symmetry Plane  Sang Woo Lee, Sang Won Park, Kumoh National University of Technology, Kyungbook, Korea; Joon Sik Lee, Seoul National University, Seoul, Korea    2000-GT-0256 
IGTI  2000  Flow Characteristics Inside Circular Injection Holes Normally Oriented to a Crossflow: Part II - Three Dimensional Flow Data and Aerodynamic Loss  Sang Woo Lee, Seong Kuk Joo, Kumoh National University of Technology, Kyungbook, Korea; Joon Sik Lee, Seoul National University, Seoul, Korea    2000-GT-0257 
IGTI  2000  Aerodynamic Loss Characteristics of a Turbine Blade with Trailing Edge Coolant Ejection Part 2: External Aerodynamics, Total Pressure Losses and Predictions  Oguz Uzol, Cengiz Camci, The Pennsylvania State University, University Park, PA, USA    2000-GT-0258 
IGTI  2000  Measurements in Separated and Transitional Boundary Layers Under Low-Pressure Turbine Airfoil Conditions  Ralph J. Volino, United States Naval Academy, Annapolis, MD, USA; Lennart S. Hultgren, NASA Glenn Research Center at Lewis Field, Cleveland, OH, USA    2000-GT-0260 
IGTI  2000  High Lift and Aft Loaded Profiles for Low Pressure Turbines  R.J. Howell, O.N. Ramesh, H.P. Hodson, Whittle Laboratory, University of Cambridge, Cambridge, UK; N.W. Harvey, Rolls-Royce plc., Derby, UK; V. Schulte, BMW Rolls-Royce, GmbH, Dahlewitz, Germany    2000-GT-0261 
IGTI  2000  Turbine Separation Control Using Pulsed Vortex Generator Jets  Jeffrey P. Bons, Air Force Institute of Technology, Wright-Patterson AFB, OH, USA; Rolf Sondergaard, Richard B. Rivir, Air Force Research Laboratory, Wright-Patterson AFB, OH, USA    2000-GT-0262 
IGTI  2000  Effects of Reynolds Number and Free Stream Turbulence on Boundary Layer Transition in a Compressor Cascade  Heinz-Adolf Schreiber, Wolfgang Steinert, German Aerospace Center (DLR) Institute of Propulsion Technology, Köln, Germany; Bernhard Küsters, Siemens AG Power Generation (KWU), Mülheim a.d. Ruhr, Germany    2000-GT-0263 
IGTI  2000  Natural Transition Phenomena on an Axial Compressor Blade  J.D. Hughes, G.J. Walker, University of Tasmania, Hobart, Australia    2000-GT-0264 
IGTI  2000  Turbine Blade Entropy Generation Rate Part I: The Boundary Layer Defined  M.R.D. Davies, F.K. O'Donnell, A.J. Niven, University of Limerick, Limerick, Ireland    2000-GT-0265 
IGTI  2000  Turbine Blade Entropy Generation Rate Part II: The Measured Loss  F.K. O'Donnell, M.R.D. Davies, University of Limerick, Limerick, Ireland    2000-GT-0266 
IGTI  2000  Control of Separation Bubble on a Blade Leading Edge by a Stationary Bar Wake  K. Funazaki, Y. Harada, E. Takahashi, Iwate University, Morioka, Japan    2000-GT-0267 
IGTI  2000  Comparison of Two Highly Loaded Low Pressure Turbine Cascades Under the Influence of Wake-Induced Transition  Stefan Brunner, Leonhard Fottner, Universität der Bundeswehr München, Neubiberg, Germany; Heinz-Peter Schiffer, BMW Rolls-Royce GmbH, Dahlewitz, Germay    2000-GT-0268 
IGTI  2000  Experimental and Numerical Investigation of Wake-Induced Transition on a Highly Loaded LP Turbine at Low Reynolds Numbers  Peter Stadtmüller, Leonhard Fottner, Universität der Bundeswehr München, Neubiberg, Germany; Andreas Fiala, MTU Motoren-und Turbinen-Union München GmbH, München, Germany    2000-GT-0269 
IGTI  2000  Separation Bubbles Under Steady and Periodic-Unsteady Main Flow Conditions  Weiliang Lou, Jean Hourmouziadis, Berlin University of Technology, Berlin, Germany    2000-GT-0270 
IGTI  2000  The Influence of Multimode Transition Initiated by Periodic Wakes on the Profile Loss of a Linear Compressor Cascade  Reinhold Teusch, Stefan Brunner, Leonhard Fottner, Universität der Bundeswehr München, Neubiberg, Germany; Marius Swoboda, BMW Rolls-Royce AeroEngines, Dahlewitz, Germany    2000-GT-0271 
IGTI  2000  Studies on Turbulence Structure of Boundary Layers Disturbed by Moving Wakes  K. Funazaki, Y. Aoyama, Iwate University, Morioka, Japan    2000-GT-0272 
IGTI  2000  Effects of Turbulence and Solidity on the Boundary Layer Development in a Low Pressure Turbine  W.J. Solomon, General Electric Aircraft Engines, Cincinnati, OH, USA    2000-GT-0273 
IGTI  2000  A Study on Models to Simulate Boundary Layer Transition in Turbomachinery Flows  M. Müller, H.E. Gallus, R. Niehuis, Institut für Strahlantriebe und Turboarbeitsmaschinen, Aachen, Germany    2000-GT-0274 
IGTI  2000  Numerical and Experimental Investigation of Low Reynolds Number Effects on Laminar Flow Separation and Transition in a Cascade of Compressor Blades  Shunji Enomoto, National Aerospace Laboratory, Tokyo, Japan; C. Hah, NASA Glenn Research Center, Cleveland, OH, USA; G.V. Hobson, Naval Postgraduate School, Monterey, CA, USA    2000-GT-0276 
IGTI  2000  Prediction of a Laminar Separation Bubble Over a Controlled-Diffusion Compressor Blade  G.V. Hobson, S. Weber, Naval Postgraduate School, Monterey, CA, USA    2000-GT-0277 
IGTI  2000  Bypass Transition Modelling: A New Method which Accounts for Free-Stream Turbulence Intensity and Length Scale  Paul E. Roach, ABB Alstom Power, Lincoln, UK; David H. Brierley, Rolls-Royce plc, Derby, UK    2000-GT-0278 
IGTI  2000  Droplet Generation by Disintegration of Oil Films at the Rim of a Rotating Disk  A. Glahn, M.F. Blair, UTRC, East Hartford, CT, USA; S. Busam, S. Wittig, Universität Karlsruhe, Karlsruhe, Germany; K.L. Allard, Pratt & Whitney, East Hartford, CT, USA    2000-GT-0279 
IGTI  2000  Flow Visualisation in a Rotating Cavity with Axial Throughflow  Dieter E. Bohn, Gregor N. Deutsch, Aachen University of Technology, Aachen, Germany; Burkhard Simon, Claus Burkhardt, DaimlerChrysler Aerospace MTU München GmbH, Munich, Germany    2000-GT-0280 
IGTI  2000  Flow and Heat Transfer in a Rotating Cavity with a Stationary Stepped Casing  Abdul A. Jaafar, Michael Wilson, J. Michael Owen, University of Bath, Bath, UK; Fariborz Motallebi, Queen Mary & Westfield College, London, UK    2000-GT-0281 
IGTI  2000  Conjugate Heat Transfer Analysis of an Engine Internal Cavity  A. Montenay, L. Paté, JM. Duboué, Snecma, Moissy-Cramayel, France    2000-GT-0282 
IGTI  2000  Total Pressure Losses in Rotor Systems with Radial Inflow  D. Brillert, H. Simon, University of Duisburg, Duisburg, Germany; D. Lieser, A.W. Reichert, Siemens AG, Mülheim, Germany    2000-GT-0283 
IGTI  2000  Experimental and Numerical Investigation of the Influence of Rotor Blades on Hot Gas Ingestion into the Upstream Cavity of an Axial Turbine Stage  Dieter Bohn, Bernd Rudzinski, Norbert Sürken, Aachen University of Technology, Aachen, Germany; Wolfgang Gärtner, DaimlerChrysler Aerospace MTU München GmbH, München, Germany    2000-GT-0284 
IGTI  2000  Flow and Heat Transfer in an Industrial Rotor-Stator Rim Sealing Cavity  Alexander V. Mirzamoghadam, Zhenhua Xiao, Siemens Westinghouse Power Corporation, Orlando, FL, USA    2000-GT-0285 
IGTI  2000  Experimental Analysis of the Effect of Swirl on the Pressure Field in Whirling 50% Eccentric Annular Seal  Bernard Robic, ABB Alstom Power, Baden, Switzerland; Gerald Morrison, Texas A&M University, College Station, TX, USA    2000-GT-0286 
IGTI  2000  Influence of a Honeycomb Facing on the Heat Transfer in a Stepped Labyrinth Seal  K. Willenborg, V. Schramm, S. Kim, S. Wittig, Universität Karlsruhe, Karlsruhe, Germany    2000-GT-0290 
IGTI  2000  Influence of a Honeycomb Facing on the Flow Through a Stepped Labyrinth Seal  V. Schramm, K. Willenborg, S. Kim, S. Wittig, Universität Karlsruhe, Karlsruhe, Germany    2000-GT-0291 
IGTI  2000  Computed Effect of Rub-Groove Size on Stepped Labyrinth Seal Performance  David L. Rhode, Texas A&M University, College Station, TX, USA; Richard G. Adams, Texaco E&P, Inc., New Orleans, LA, USA    2000-GT-0292 
IGTI  2000  Large Scale Testing to Validate the Influence of External Crossflow on the Discharge Coefficients of Film Cooling Holes  D.A. Rowbury, Rolls-Royce plc, Bristol, UK; M.L.G. Oldfield, University of Oxford, Oxford, UK; G.D. Lock, University of Bath, Bath, UK    2000-GT-0293 
IGTI  2000  A Method for Correlating the Influence of External Crossflow on the Discharge Coefficients of Film Cooling Holes  D.A. Rowbury, Rolls-Royce plc, Bristol, UK; M.L.G. Oldfield, University of Oxford, Oxford, UK; G.D. Lock, University of Bath, Bath, UK    2000-GT-0294 
IGTI  2000  Systematic Experimental and Numerical Investigations on the Aerothermodynamics of a Film Cooled Turbine Cascade with Variation of the Cooling Hole Shape Part I Experimental Approach  Wolfgang Ganzert, Leonhard Fottner, Universität der Bundeswehr München, Neubiberg, Germany; Thomas Hildebrandt, NUMECA, Wendelstein, Germany    2000-GT-0295 
IGTI  2000  A Presentation of Detailed Experimental Data of a Suction Side Film Cooled Turbine Cascade  Holger Brandt, Wolfgang Ganzert, Leonhard Fottner, Universität der Bundeswehr München, Neubiberg, Germany    2000-GT-0296 
IGTI  2000  Film Cooling Jet Aerodynamics for a Pipe and a Converging Nozzle Injection Hole  Jun Sasahara, Takaaki Shizawa, Shinji Honami, Science University of Tokyo, Tokyo, Japan; Yukiko Suzuki, Transportation Bureau of Tokyo Metropolitan Government, Tokyo, Japan; Shigeru Tanaka, JGC Corporation, Kanagawa, Japan    2000-GT-0297 
IGTI  2000  Systematic Experimental and Numerical Investigations on the Aerothermodynamics of a Film Cooled Turbine Cascade with Variation of the Cooling Hole Shape Part II Numerical Approach  Thomas Hildebrandt, NUMECA Ing.-Büro, Wendelstein, Germany; Wolfgang Ganzert, Leonhard Fottner, Universität der Bundeswehr München, Neubiberg, Germany    2000-GT-0298 
IGTI  2000  Strategy for a Cost Optimized Operation of a Flexible Cogenration Gas Turbine Plant  D. Hein, K. Kwanka, M. Nixdorf, Technische Universität München, Garching, Germany    2000-GT-0299 
IGTI  2000  Spinning Reserve Influence in a Power Generating System Integrated by Hydro Storage Plants  M. Bianchi, E. Gadda, A. Peretto, DIEM - University of Bologna, Bologna, Italy    2000-GT-0300 
IGTI  2000  Selection of Cycle Configurations for Combined Cycle Cogeneration Power Plants  Rattan Tawney, John Ehman, Mona Brown, Becthel Power Corporation, Frederick, MD, USA    2000-GT-0301 
IGTI  2000  PEACES: A Program for the Economic Analysis of Combined Energy Systems  Joseph Roy-Aikins, University of Durban-Westville, Durban, South Africa    2000-GT-0302 
IGTI  2000  Application of Evaporative Coolers for Gas Turbine Power Plants  J. Douglas McNeilly, Enron Engineering & Construction Company, Houston, TX, USA    2000-GT-0303 
IGTI  2000  Evaluation of Operational Performance of a Gas Turbine Cogeneration Plant with Intake Air Cooled by Ice Storage  Ryohei Yokoyama, Koichi Ito, Osaka Prefecture University, Osaka, Japan    2000-GT-0304 
IGTI  2000  Fog System Performance in Power Augmentation of Heavy Duty Power Generating Gas Turbines Model 7EA  Steve Ingistov, ARCO/WCC, Carson, CA, USA    2000-GT-0305 
IGTI  2000  Modular Uprating and Upgrading Solutions in ABB ALSTOM POWER Gas Turbines  Wilfried De Backer, Carsten Bopp, ABB Alstom Power, Baden, Switzerland    2000-GT-0306 
IGTI  2000  Inlet Fogging of Gas Turbine Engines - Part A: Theory, Psychrometrics, and Fog Generation  Cyrus B. Meher-Homji, Bechtel Corporation, Houston, TX, USA; Thomas R. Mee III, Mee Industries Inc., Monrovia, CA, USA    2000-GT-0307 
IGTI  2000  Inlet Fogging of Gas Turbine Engines - Part B: Practical Considerations, Control and O&M Aspects  Cyrus B. Meher-Homji, Bechtel Corporation, Houston, TX, USA; Thomas R. Mee III, Mee Industries Inc., Monrovia, CA, USA    2000-GT-0308 
IGTI  2000  Set-up of an Adaptive Method for the Diagnosis of Gas Turbine Operating State by Using Test-Bench Measurements  R. Bettocchi, University of Ferrara, Ferrara, Italy; P.R. Spina, DIEM - University of Bologna, Bologna, Italy; E. Benvenuti, Nuovo Pignone S.p.A., Firenze, Italy    2000-GT-0309 
IGTI  2000  Optimum Management System with Environmental Monitoring  G. Cerri, B. Seyedan, Università Degli Studi Roma TRE, Rome, Italy; R. Evans, Unversity of Ulster, Coleraine, UK; C.A. Frangopolous, National Technical University of Athens, Athens, Greece; M. Parrella, Gap Gemini Italia S.p.A., Roma, Italy; R.U. Pitt, Fa    2000-GT-0310 
IGTI  2000  Gas Turbine Field Performance Determination: Sources of Uncertainties  M. Pinelli, University of Ferrara, Ferrara, Italy; P.R. Spina, DIEM - University of Bologna, Bologna, Italy    2000-GT-0311 
IGTI  2000  Real-Time On-Line Performance Diagnostics of Heavy-Duty Industrial Gas Turbines  S. Can Gülen, Patrick R. Griffin, Thermoflow Incorporated, Sudbury, MA, USA; Sal Paolucci, General Electric Company, Indian Orchard, MA, USA    2000-GT-0312 
IGTI  2000  Influence of Ambient Conditions on an Aeroderivative Gas Turbine Based Cogeneration Plant - A Comparison of Numerical Simulation with Field Performance Data  Carlo Carcasci, Bruno Facchini, Francesco Grillo, Universtià di Firenze, Firenze, Italy    2000-GT-0313 
IGTI  2000  Remote Monitoring & Diagnostics System for GE Heavy Duty Gas Turbines  Dincer Ozgur, Richard Rucigay, Arkalgud N. Lakshminarasimha, GE Power Systems, Atlanta, GA, USA; Mahesh Morjaria, S. Sanborn, GE Corporate Research & Development, Schenectady, NY, USA    2000-GT-0314 
IGTI  2000  Inverted Brayton Cycle Employment for Low Temperature Cogenerative Applications  M. Bianchi, G. Negril di Montenegro, A. Peretto, University of Bologna, Bologna, Italy    2000-GT-0315 
IGTI  2000  Thermo-Economic Analysis of an Intercooled, Reheat and Recuperated Gas Turbine for Cogeneration Applications: Part I - Base Load Operation  R. Bhargava, Universal Ensco, Inc., Houston, TX, USA; M. Bianchi, G. Negril di Montenegro, A. Peretto, University of Bologna, Bologna, Italy    2000-GT-0316 
IGTI  2000  Utilization of Cryogenic Exergy of LNG by MGT (Mirror Gas Turbine)  Y. Tsujikawa, K. Kaneko, S. Fujii, Osaka Prefecture University, Osaka, Japan    2000-GT-0317 
IGTI  2000  Performance Prediction of Small Scale Tri-Generation Plants Based on Integrated SOFC and Microturbine Systems  Stafano Campanari, Ennio Macchi, Politecnico di Milano, Milano, Italy    2000-GT-0318 
IGTI  2000  Evaluation of Cyclic Operation of Heat Recovery Steam Generators- A Practical Approach  Lewis Douglas, Joseph E. Schroeder, Vernon L. Eriksen, Nooter/Eriksen, Inc., St. Louis, MO, USA    2000-GT-0319 
IGTI  2000  A Steady State Calculation Model for Gas Turbine Thermal Enclosures  Umberto Desideri, Francesco Di Maria, Università di Perugia, Perugia, Italy    2000-GT-0320 
IGTI  2000  Design Implementation of the Intercooler System of the WR-21  Phil A. Cabanos, Northrop Grumman Marine Systems, Sunnyvale, CA, USA    2000-GT-0321 
IGTI  2000  Numerical and Experimental Study on the Suppression for the Infared Signatures of a Marine Gas Turbine Exhaust System  Zhou Shaorong, Du Zhaohui, Chen Hanping, Zhong Fangyuan, Shanghai Jiao Tong University, Shanghai, China    2000-GT-0322 
IGTI  2000  The Design and Implementation of a PLC Based Gas Turbine Controller for a Shipboard Application  Vincent P. Tolotta, Naval Surface Warfare Center, Philadelphia, PA, USA    2000-GT-0323 
IGTI  2000  Digital Controls and Modern Fuel Systems for Marine Prime Movers  Philip R. Bellio, Woodward Industrial Controls, Fort Collins, CO, USA    2000-GT-0324 
IGTI  2000  Influence of Disturbances on Transients of a Gas Turbine Ship Propulsion System - Preliminary Investigations  Marek Dzida, Zygfryd Domachowski, Technical University of Gdansk, Gdansk, Poland    2000-GT-0325 
IGTI  2000  U.S. Navy Shipboard Fleet Evaluation of the Redundant Independent Mechanical Start System and Full Authority Digital Control  Matthew G. Hoffman, Helen J. Kozuhowski, Naval Surface Warfare Center, Philadelphia, PA, USA; Leonard L. Overton, Jr., Rolls-Royce Allison, Indianapolis, IN, USA    2000-GT-0326 
IGTI  2000  Gas Turbine Control System Integration for Royal Caribbean Millennium Class Cruise Liner  David J. Olsheski, William W. Schulke, Woodward Industrial Controls, Fort Collins, CO, USA    2000-GT-0327 
IGTI  2000  Water Mist Fire-Fighting System in the Marine LM2500 Gas Turbine Module  Glenn McAndrews, GE Marine Engines, Cleveland, OH, USA; Victor M. Gameiro, Securiplex Inc., Dorval, PQ, Canada; Tom Shirriff, Canadian Navy, Ottawa, ON, Canada    2000-GT-0328 
IGTI  2000  Italian Navy Evaluation Concerning the Use of Electronic Fuel Control and Hydraulic Starters for Fiat - GE LM2500 Gas Turbine  Massimo Maggini, Michele Giuliano, Italian Navy General Staff, Rome, Italy    2000-GT-0329 
IGTI  2000  A Low Temperature CVD Process for Aluminum & Aluminide Coatings  J. Liburdi, P. Lowden, V. Moravek, Liburdi Engineering Limited, Dundas, Ontario, Canada    2000-GT-0330 
IGTI  2000  Cyclic Oxidation of a NiCoCrAly Coating Applied by HVOF & LPPS  Henry L. Bernstein, Peggy L. Talley, Gas Turbine Materials Associates, San Antonio, TX, USA; Wayne L. Greaves, Hans van Esch, Hickham Industries, Inc., LaPorte, TX, USA    2000-GT-0332 
IGTI  2000  Improved Processing Route for Aluminization of Gas Turbine Components  Thomas A. Kircher, David Solovei, Sermatech Maine, Biddeford, ME, USA; Joseph H. Steck, Srinivasan "Shanks" Shankar, TFX Sermatech, Limerick, PA, USA    2000-GT-0333 
IGTI  2000  Effect of Crystal Orientation on Fatigue Failure of Single Crystal Nickel Base Turbine Blade Superalloys  Nagaraj K. Arakere, University of Florida, Gainesville, FL, USA; Gregory Swanson, NASA Marshall Space Flight Center, MSFC, AL, USA    2000-GT-0334 
IGTI  2000  The Effect of Primary Axis and Low Angle Boundary Misorientation on CMSX-10K Mechanical Properties  Yakin Patel, Paul F. Browning, Michael D. Fitzpatrick, Solar Turbines Incorporated, San Diego, CA, USA; Dean Schmiedechnekt, Allen Price, Tammy Simpson, Howmet Corporation, Whitehall, MI, USA; Gary Erickson, Ken Harris, Cannon-Muskegon Corp., Muskegon, MI    2000-GT-0335 
IGTI  2000  Fracture Toughness Properties of a Modern Ni-Mo-Cr High Temperature Alloy  R.R. Seeley, D.L. Klarstrom, Haynes International, Inc., Kokomo, IN, USA    2000-GT-0336 
IGTI  2000  High Temperature Brazing for Cobalt-Based Gas Turbine Components  Wayne Greaves, Hans van Esch, Hickham Industries, Inc., La Porte, TX, USA    2000-GT-0337 
IGTI  2000  Fluoride Ion Cleaning (FIC) at Sub-Atmospheric Pressure  Warren Miglietti, Sermatech International, Inc., Manchester, CT, USA; Tom Cullen, Ti-Coatings, Inc., Utica, MI, USA    2000-GT-0338 
IGTI  2000  Liquid Phase Diffusion Bond Repair of Westinghouse 501F, Row 3 Vanes  Warren M. Miglietti, Rich Curtis, Brandon Hall, Christina M. Lazarin, Sermatech International, Inc., Manchester, CT, USA    2000-GT-0339 
IGTI  2000  Adaptive Strategies for Manufacturing and Repair of Blades and Blisks  Claus Bremer, BCT GmbH, Dortmund, Germany    2000-GT-0340 
IGTI  2000  New Cost Effective Milling Technologies for Manufacturing Blisks.  Richard M. Bacon, Starrag Worldwide, Rorschacherberg, Switzerland    2000-GT-0341 
IGTI  2000  A Study on Five-Axis Flank Machining of Centrifugal Compressor Impellers  Der Min Tsay, Huo Chu Chen, Ming Jane Her, National Sun Yat Sen University, Kaohsiung, Taiwan    2000-GT-0342 
IGTI  2000  Investigation Concerning the Aerothermodynamic Performance Perturbation of a 19MW Intercooled Air Compressor  Inam U. Haq, SABIC Research & Technology, Jubail, Saudi Arabia; Ali H. Al-Jameel, Khalid N. Al-Khalidi, National Industrial Gases Company (GAS), Jubail, Saudi Arabia    2000-GT-0343 
IGTI  2000  Development of High Tech and Increased Efficiency Retrofit Options for the GE MS3002 Gas Turbine  A. Coppola, S. Francini, F. Noera, GEPS Nuovo Pignone, Florence, Italy    2000-GT-0344 
IGTI  2000  Degradation in Gas Turbine Systems  Rainer Kurz, Klaus Brun, Solar Turbines Incorporated, San Diego, CA, USA    2000-GT-0345 
IGTI  2000  Advanced Oil Debris Monitoring for Pipeline Mechanical Drive Gas Turbines  Duka Kitaljevich, GasTOPS Ltd., Gloucester, ON, Canada; Gerrit J. van Veldhuizen, Thomassen International bv, Rheden, Netherlands    2000-GT-0347 
IGTI  2000  Energy Optimisation and Reduction of CO2-Emission on the North Sea Sleipner Gas Production Platform  Harald Underbakke, Jon Jakobsen, Statoil, Stavanger, Norway    2000-GT-0348 
IGTI  2000  Microphone Probe for In-Duct Measurement of Gas Turbine Exhaust Noise  M.P. Sacks, R. Behboudi, Tacet Engineering Ltd., Toronto, ON, Canada; J.G. Kawall, Ryerson Polytechnic University, Toronto, ON, Canada; J. Buttell, Higgot-Kane Industrial Noise Controls Ltd., Pickering, ON, Canada    2000-GT-0349 
IGTI  2000  CFD Predictions and Field Measurements of NOx Emissions from LM1600 Gas Turbine During Part Load Operation  G.R. Price, K.K. Botros, NOVA Research & Technology Centre, Calgary, Canada; G.M. Goldin, Fluent Inc., Lebanon, NH, USA    2000-GT-0350 
IGTI  2000  A Demonstration of Artificial Neural Networks Based Data Mining for Gas Turbine Driven Compressor Stations  K.K. Botros, NOVA Research & Technology Corporation, Alberta, Canada; G. Kibrya, A. Glover, TransCanada Pipelines, Ltd., Alberta, Canda    2000-GT-0351 
IGTI  2000  An Innovative Device for Passive Control of Surge in Industrial Compression Systems  Gianmario L. Arnulfi, Pietro Giannattasio, Piero Pinamonti, University of Udine, Udine, Italy; Diego Micheli, University of Trieste, Trieste, Italy    2000-GT-0352 
IGTI  2000  Model-Based Detection of Leaks and Blockages in Pipes  Anju Narendra, John Down, Kirk Mathews, Ravi Rajamani, GE Corporate Research & Development, Schenectady, NY, USA; Sal Leone, Jonathan Thatcher, Bruce Norman, GE Power Systems, Schenectady, NY, USA    2000-GT-0353 
IGTI  2000  Active Controlled Hydrostatic Bearings for a New Generation of Machines  Donald E. Bently, John W. Grant, Phillip C. Hanifan, Bently Nevada Corporation, Minden, NV, USA    2000-GT-0354 
IGTI  2000  A Scientific Approach to the Process Development of Bonded Attachments for High Speed Rotor Application  Ronald R. Cairo, Pratt & Whitney, West Palm Beach, FL, USA; Kathleen A. Sargent, Air Force Research Laboratory, Wright-Patterson AFB, OH, USA    2000-GT-0355 
IGTI  2000  Contact Stresses in Dovetail Attachments: Physical Modeling  G.B. Sinclair, N.G. Cormier, Carnegie Mellon University, Pittsburgh, PA, USA    2000-GT-0356 
IGTI  2000  Simulation of the Rotational Vibration Response of a Spur Gear Pair with One Cracked Tooth  Sidi M. Berri, J.M Klosner, Polytechnic University, Farmingdale, NY, USA    2000-GT-0357 
IGTI  2000  Experimental Investigation of Mode Localization and Forced Response Amplitude Magnification for a Mistuned Bladed Disk  John Judge, Christophe Pierre, University of Michigan, Ann Arbor, MI, USA; Oral Mehmed, NASA Glenn Research Center, Cleveland, OH, USA    2000-GT-0358 
IGTI  2000  A Novel Technique for the Measurement of Blade Damping Using Piezoelectric Actuators  T.R. Jeffers, J.J. Kielb, Ohio State University, Columbus, OH, USA; R.S. Abhari, Swiss Federal Institute of Technology, Zurich, Switzerland    2000-GT-0359 
IGTI  2000  Component-Mode-Based Reduced Order Modeling Techniques for Mistuned Bladed Disks, Part I: Theoretical Models  Ronnie Bladh, Matthew P. Castanier, Christophe Pierre, University of Michigan, Ann Arbor, MI, USA    2000-GT-0360 
IGTI  2000  Component-Mode-Based Reduced Order Modeling Techniques for Mistuned Bladed Disks, Part II: Application  Ronnie Bladh, Matthew P. Castanier, Christophe Pierre, University of Michigan, Ann Arbor, MI, USA    2000-GT-0361 
IGTI  2000  A Comparison of Two Finite Element Reduction Techniques for Mistuned Bladed-Disks  François Moyroud, Torsten Fransson, Royal Institute of Technology, Stockholm, Sweden; Georges Jacquet-Richardet, Institut National des Sciences Appliquées de Lyon, Villeurbanne, France    2000-GT-0362 
IGTI  2000  Friction Damper Mistuning of a Bladed Disk and Optimization with Respect to Wear  Martin H. Jareland, Linköping University, Linköping, Sweden; Gabor Csaba, Volvo Aero Corporation, Trollhättan, Sweden    2000-GT-0363 
IGTI  2000  Limit Cycle Due to Interlocked Shroud Friction: Instrumental to the High-Bypass Turbofan  Nicholas Klompas, Waterford, NY, USA    2000-GT-0364 
IGTI  2000  On the Application of Powder Shear Damping to a Structural Element  Erik E. Swanson, Thomas E. Russell III, James Walton II, David S. Xu, Hooshang Heshmat, Mohawk Innovative Technology, Inc., Albany, NY, USA    2000-GT-0365 
IGTI  2000  Development of a Passive Turbine Blade Damper Using Magnetomechanical Coating  H.-Y. Yen, M.-H. Herman Shen, The Ohio State University, Columbus, OH, USA    2000-GT-0366 
IGTI  2000  Experimental Determination of Powder Film Shear and Damping Characteristics  Hooshang Heshmat, Mohawk Innovative Technology, Inc., Albany, NY, USA    2000-GT-0368 
IGTI  2000  Mode Localization in a Grouped Bladed Disk  J.H. Kuang, National Sun Yat-Sen University, Kaohsiung, Taiwan; B.W. Huang, Cheng Shiu Institute of Technology, Kaohsiung, Taiwan    2000-GT-0369 
IGTI  2000  A Resonance Tracking Algorithm for the Prediction of Turbine Forced Response with Friction Dampers  C. Bréard, M. Vahdati, M. Imregun, Imperial College of Science, Technology & Medicine, London, UK; J.S. Green, Rolls-Royce plc, Derby, UK    2000-GT-0372 
IGTI  2000  An Integrated Time-Domain Aeroelasticity Model for the Prediction of Fan Forced Response Due to Inlet Distortion  C. Bréard, M. Vahdati, A.I. Sayma, M. Imregun, Imperial College of Science, Technology & Medicine, London, UK    2000-GT-0373 
IGTI  2000  Prediction of Low Engine Order Inlet Distortion Driven Resonance in a Low Aspect Ratio Fan  J.G. Marshall, J.W. Chew, Rolls-Royce plc, Derby, UK; L. Xu, J. Denton, Whittle Laboratory, Cambridge University, Cambridge, UK    2000-GT-0374 
IGTI  2000  Forcing Function Measurements and Predictions of a Transonic Vaneless Counter Rotating Turbine  Matthew M. Weaver, Reza S. Abhari, Michael G. Dunn, Ohio State University, Columbus, OH, USA; Steven R. Manwaring, Michael J. Salay, GE Aircraft Engines, Cincinnati, OH, USA; Kuk K. Frey, Nathan Heidegger, Rolls Royce Allison, Indianapolis, IN, USA    2000-GT-0375 
IGTI  2000  Interaction Effects in a Transonic Stage  J.W. Barter, GE Aircraft Engines, Cincinnati, OH, USA; P.H. Vitt, ASE Technologies, Cincinnati, OH, USA; J.P. Chen, Mississippi State University, Mississippi State, MS, USA    2000-GT-0376 
IGTI  2000  Application of Model Order Reduction to Compressor Aeroelastic Models  Karen Willcox, Jaime Peraire, James D. Paduano, Massachusetts Institute of Technology, Cambridge, MA, USA    2000-GT-0377 
IGTI  2000  Experimental Investigation of Shock-Induced Blade Oscillation at an Elastically Suspended Turbine Cascade in Transonic Flow  Brigitte Urban, Heinz Stetter, University of Stuttgart, Stuttgart, Germany; Nicolas Vortmeyer, Siemens AG, KWU Group, Muelheim, Germany    2000-GT-0378 
IGTI  2000  Sensitivity Analysis of Blade Mode Shape on Flutter of Two-Dimensional Turbine Blade Sections  Olga V. Tchernycheva, Sébastien Regard, François Moyroud, Torsten H. Fransson, Royal Institute of Technology, Stockholm, Sweden    2000-GT-0379 
IGTI  2000  A Coupled Fluid-Structure Analysis for 3D Flutter in Turbomachines  Vitaly Gnesin, Luba Kolodyazhnaya, Ukrainian National Academy of Sciences, Kharkov, Ukraine; Romuald Rzadkowski, Polish Academy of Sciences, Gdansk, Poland    2000-GT-0380 
IGTI  2000  Numerical Investigation of Nonlinear Fluid-Structure Interaction in Vibrating Compressor Blades  Volker Carstens, Joachin Belz, Institute of Aeroelasticity DLR, Göttingen, Germany    2000-GT-0381 
IGTI  2000  A Novel Post-processing Platform for 2D Steady and Unsteady Flows in Turbomachines  François Moyroud, Torsten H. Fransson, Royal Institute of Technology, Stockholm, Sweden    2000-GT-0382 
IGTI  2000  The Impact of Viscous Effects on the Aerodynamic Damping of Vibrating Transonic Compressor Blades - A Numerical Study  Björn Grüber, Daimler Chrysler Aerospace, Munich, Germany; Volker Carstens, Institute of Aeroelasticity DLR, Göttingen, Germany    2000-GT-0383 
IGTI  2000  Parametric Study of the Pressure Stability on an Oscillating Airfoil from Stable to Stalled Flow Conditions  S. Svensdotter, T. Fransson, Royal Institute of Technology, Stockholm, Sweden; U. Johansson, Volvo Aero Corporation, Trollhättan, Sweden    2000-GT-0384 
IGTI  2000  A Navier-Stokes Analysis of the Stall Flutter Characteristics of the Buffum Cascade  Stefan Weber, Max F. Platzer, Naval Postgraduate School, Monterey, CA, USA    2000-GT-0385 
IGTI  2000  Synchronous Instability Problems in High Performance Turbomachines During Steady State Full Load Operation  Inam U. Haq, SABIC Research & Technology, Jubail, Saudi Arabia; Chittineni V. Kumar, Adel H. Basheer, Al-Jubail Fertilizers Company, Jubail, Saudi Arabia    2000-GT-0386 
IGTI  2000  Capabilities of Large Foil Bearings  Erik E. Swanson, Hooshang Heshmat, Mohawk Innovative Technology, Inc., Albany, NY, USA    2000-GT-0387 
IGTI  2000  Dynamic Response of a Rotor-Integral Squeeze Film Damper to Couple Imbalances  Oscar De Santiago, Luis San Andrés, Texas A&M University, College Station, TX, USA    2000-GT-0388 
IGTI  2000  Rotor/Seal Experimental and Analytical Study on Full Annular Rub  John J. Yu, Paul Goldman, Donald E. Bently, Bently Rotor Dynamics Research Corporation, Minden, NV, USA    2000-GT-0389 
IGTI  2000  Dynamics and Stability of Rotor/Stator Systems with Rubs  Jun Jiang, Heinz Ulbrich, University of Essen, Essen, Germany    2000-GT-0390 
IGTI  2000  Rolling Element Bearing Non-Linearity Effects  N.S. Feng, E.J. Hahn, The University of New South Wales, Sydney, Australia    2000-GT-0391 
IGTI  2000  Multilevel Optimization of Rotor Bearing System with Dynamic Behavior Constraints  T.N. Shiau, H.J. Lee, Y.J. Tsai, National Chung Cheng University, Chia-Yi, Taiwan    2000-GT-0392 
IGTI  2000  Instability of an Over-Hung Rigid Centrifuge Rotor Partially Filled with Fluid  Zhu Changsheng, Zhejiang University, Zhejiang, China; H. Ulbrich, University of Essen, Essen, Germany    2000-GT-0393 
IGTI  2000  Orbit-Based Identification of Damping Coefficients from a Rotor Mounted on Off-Centered Squeeze Film Dampers and Including Support Flexibility  Sergio Diaz, Luis San Andrés, Texas A&M University, College Station, TX, USA    2000-GT-0394 
IGTI  2000  Reconciliation of Rotordynamic Models with Experimental Data  Eric H. Maslen, José A. Vázquez, University of Virginia, Charlottesville, VA, USA; Christopher K. Sortore, Synchrony, Inc., Roanoke, VA, USA    2000-GT-0395 
IGTI  2000  Synchronous Response Estimation in Rotating Machinery  Eric H. Maslen, José A. Vázquez, Carl R. Knospe, University of Virginia, Charlottesville, VA, USA; Christopher K. Sortore, Synchrony, Inc., Roanoke, VA, USA    2000-GT-0397 
IGTI  2000  Measurements of Rotordynamic Coefficients of Hybrid Bearings with: (a) A Plugged Orifice, and (b) A Worn Land Surface  Franck Laurant, Warwick, RI, USA; Dara W. Childs, Texas A&M University, College Station, TX, USA    2000-GT-0398 
IGTI  2000  Experimental and Theorectical Comparison of Two Swirl Brake Designs  K.K. Nielsen, C.M. Myllerup, Ødegaard & Danneskiold- Samsøe A/S, Copenhagen, Denmark; D.W. Childs, Texas A&M University, College Station, TX, USA    2000-GT-0399 
IGTI  2000  Identification of Bearing Coefficients of Flexible Rotor-Bearing Systems  Tachung Yang, Wei-Ching Chaung, Yuan Ze University, Taoyuan, Taiwan    2000-GT-0400 
IGTI  2000  The Effect of Viscous and Hysteretic Damping on Rotor Stability  Anthony M. Cerminaro, The Charles Stark Draper Laboratory, Cambridge, MA, USA; Frederick C. Nelson, Tufts University, Medford, MA, USA    2000-GT-0401 
IGTI  2000  A New CFD-Perturbation Model for the Rotordynamics of Incompressible Flow Seals  Namhyo Kim, David H. Rhode, Texas A&M University, College Station, TX, USA    2000-GT-0402 
IGTI  2000  Dynamic Coefficients of Labyrinth Gas Seals - A Comparison of Experimental Results and Numerical Calculations  K. Kwanka, Technische Universität München, Germany; J. Sobotzik, R. Nordmann, Technische Universität Darmstadt, Germany    2000-GT-0403 
IGTI  2000  Flexible Bearing Supports, Using Experimental Data  José A. Vázquez, Ronald D. Flack, Lloyd E. Barrett, University of Virginia, Charlottesville, VA, USA    2000-GT-0404 
IGTI  2000  Analysis and Testing of a Magnetic Bearing Energy Storage Flywheel with Gain-Scheduled, MIMO Control  Lawrence A. Hawkins, CalNetix, Inc., Torrance, CA, USA; Brian T. Murphy, John Kajs, University of Texas, Austin, TX, USA    2000-GT-0405 
IGTI  2000  Robust Performance Analysis of Uncertain Magnetic Bearings  Toru Namerikawa, Masayuki Fujita, Kanazawa University, Kanazawa, Ishikawa, Japan    2000-GT-0406 
IGTI  2000  Three Practical Examples of Magnetic Bearing Control Design Using a Modern Tool  M. Spirig, J. Schmied, Delta JS AG, Zurich, Switzerland; P. Jenckel, U. Kanne, LUST Antriebstechnik, Lahnan, Germany    2000-GT-0407 
IGTI  2000  The µ Approach to Control of Active Magnetic Bearings  Roger L. Fittro, Aston University, Birmingham, UK; Carl R. Knospe, University of Virginia, Charlottesville, VA, USA    2000-GT-0408 
IGTI  2000  A Magnetic Bearing System for More-Electric Engines  R. Jett Field, Christopher K. Sortore, Victor Iannello, Synchrony, Inc., Roanoke, VA, USA    2000-GT-0409 
IGTI  2000  Comparison of Soft Magnetic Alloys for High Temperature Magnetic Bearings  Anthony S. Kondoleon, William P. Kelleher, Draper Laboratory, Cambridge, MA, USA    2000-GT-0410 
IGTI  2000  Performance of a Foil-Magnetic Hybrid Bearing  Erik E. Swanson, Hooshang Heshmat, James Walton II, Mohawk Innovative Technology, Inc., Albany, NY, USA    2000-GT-0411 
IGTI  2000  A New Class of Permanent Magnetic Materials for High Temperature Applications  Marlin S. Walmer, Christina H. Chen, Michael H. Walmer, Electron Energy Corporation, Landisville, PA, USA    2000-GT-0412 
IGTI  2000  The Effect of Slot Length on Flux Distribution & Rotordynamic Coefficients in Magnetic Actuators Using a Boundary Perturbation Method  Lyndon S. Stephens, University of Kentucky, Lexington, KY, USA; Mark A. Casemore, Louisiana State University, Baton Rouge, LA, USA    2000-GT-0413 
IGTI  2000  Enhancements to AMB Force Measurement Procedures for Application to a Rocket Thrust Measurement System  Joe Imlach, Imlach Consulting Engineering, Anchorage, AK, USA; Mary E.F. Kasarda, P.A. Blaji, Virginia Tech, Blacksburg, VA, USA    2000-GT-0414 
IGTI  2000  Influence Wave Mode Computations of Multi- Passage Cascade Flows  Ismail H. Tuncer, Middle East Technical University, Ankara, Turkey; Stefan Weber, Naval Postgraduate School, Monterey, CA, USA    2000-GT-0415 
IGTI  2000  Non-Uniform Flow in a Compressor Due to Asymmetric Tip Clearance  Seung Jin Song, Seung Ho Cho, Seoul National University, Seoul, Korea    2000-GT-0416 
IGTI  2000  Aerodynamic Response of Turbomachinery Blade Rows to Convecting Density Wakes  H.S. Wijesinghe, C.S. Tan, E.E. Covert, Massachusetts Institute of Technology, Cambridge, MA, USA    2000-GT-0417 
IGTI  2000  Analysis of Aerodynamically Induced Whirling Forces in Axial Flow Compressors  Z.S. Spakovszky, Massachusetts Institute of Technology, Cambridge, MA, USA    2000-GT-0418 
IGTI  2000  Elasto-Plastic and Creep Analysis of a First Stage Blade in a Land Based Gas Turbine Under Steady State Operating Conditions  Takayuki Sakai, Takashi Ogata, Akiyoshi Nomoto, Central Research Institute of Electric Power Industry, Komae Research Laboratory, Tokyo, Japan; Kazunori Watanabe, Central Research Institute of Electric Power Industry, Yokosuka Research Laboratory, Kanagaw    2000-GT-0419 
IGTI  2000  A Probabilistically-Based Damage Tolerance Analysis Computer Program for Hard Alpha Anomalies in Titanium Rotors