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Papers
Conference Year Paper Title Paper Author Page Number Other
IGTI  1992  Shock Formation In Overexpanded Tip Leakage Flow  J. Moore, Virginia Polytechnic Inst. & State University, Blacksburg, VA, USA; K.M. Elward, General Electric Company, Schenectady, NY, USA    92-GT-001 
IGTI  1992  Status Of The Automotive Ceramic Gas Turbine Development Program  T. Itoh, Japan Automobile Research Inst., Inc., Ibaraki, JAPAN; H. Kimura, Petroleum Energy Center, Tokyo, JAPAN    92-GT-002 
IGTI  1992  Current Status of 300 KW Industrial Ceramic Gas Turbine R&D In Japan  K. Honjo, R. Hashimoto, Agency of Industrial Science and Technology, MITI, Tokyo, JAPAN; H. Ogiyama, New Energy and Industrial Technology Development Organization, Tokyo, JAPAN    92-GT-003 
IGTI  1992  Recent Advances In Simulating Unsteady Flow Phenomena Brought About By Passage Of Shock Waves In A Linear Turbine Cascade  J.C. Collie, H.L. Moses, J.A. Schetz, Virginia Polytechnic Inst. & State University, Blacksburg, VA, USA; B.A. Gregory, General Electric Aircraft Engines, Cincinnati, OH, USA    92-GT-004 
IGTI  1992  A Statistical Approach To The Experimental Evaluation Of Transonic Turbine Airfoils In A Linear Cascade  M.L. Shelton, B.A. Gregory, General Electric Aircraft Engines, Cincinnati, OH, USA; R.L. Doughty, T. Kiss, H.L. Moses, Virginia Polytechnic Inst. & State University, Blacksburg, VA, USA    92-GT-005 
IGTI  1992  Coupled Multi-Disciplinary Simulation Of Composite Engine Structures In Propulsion Environment  C.C. Chamis, NASA Lewis Research Center, Cleveland, OH, USA; S.N. Singhal, Sverdrup Technology, Inc., Cleveland, OH, USA    92-GT-006 
IGTI  1992  A Study On Stability And Response Analysis Of A Nonlinear Rotor System With Mass Unbalance And Side Load  T.N. Shiau, National Cheng Kung University, Tainan, Taiwan, R.O.C.;    92-GT-007 
IGTI  1992  Investigation Of The Vibration Of A Blade With Friction Damper By HBM  J.H. Wang, W.K. Chen, National Tsing Hua University, Hsinchu, Taiwan, R.O.C.;    92-GT-008 
IGTI  1992  LQR-Based Least-Squares Output Feedback Control Of Rotor Vibrations Using The Complex Mode And Balanced Realization Methods  G.W. Fan, H.D. Nelson, P.E. Crouch, Arizona State University, Tempe, AZ, USA; M.P. Mignolet, Texas Christian University, Fort Worth, TX, USA    92-GT-009 
IGTI  1992  A Numerical Investigation Into The Nozzle Flow Of High By-Pass Turbofans  H. Zimmerman, K. Katheder, A. Jula, MTU Motoren- und Turbinen-Union München GmbH, Munich, GERMANY;    92-GT-010 
IGTI  1992  Conceptual Design Of A Centrifugal Compressor Including Consideration Of The Effect Of Inlet Prewhirl  A. Whitfield, University of Bath, Bath, UK;    92-GT-011 
IGTI  1992  Numerical Analyses Of A Rocket Engine Turbine And Comparison With Air Test Data  K. Tran, D.C. Chan, Rockwell International Corp., Canoga Park, CA, USA; S.T. Hudson, S.W. Gaddis, NASA-Marshall Space Flight Center, Huntsville, AL, USA    92-GT-012 
IGTI  1992  Analysis Of High Speed Multistage Compressor Throughflow Using Spanwise Mixing  J. Dunham, Defence Research Agency, Hampshire, UK;    92-GT-013 
IGTI  1992  Lifting Surface Theory for Steady Aerodynamic Analysis of Ducted Counter Rotation Propfan  H.K. Kodama, Ishikawajima-Harima Heavy Ind., Tokyo, JAPAN; M. Namba, Kyushu University, Fukuoka, JAPAN    92-GT-014 
IGTI  1992  Design Features Of The GTD 8000 And GTD 15000 Marine Gas Turbine Engines  V.I. Romanov, NPO Mashproject, Nicolayev, USSR;    92-GT-015 
IGTI  1992  Evaluation Of Compressor Inlet Flow Conditioners  A.H. Haidari, VORTAB, Inc., Whitehall, PA, USA; T. Hordendorf, J.C. Bartos, CONMEC, Inc., Bethlehem, PA, USA    92-GT-016 
IGTI  1992  The Influence Of Adjustable Inlet Guide Vanes On the Performance Of Multi-Stage Industrial Centrifugal Compressors  K. Ludtke, Babcock-Borsig AG, Berlin, GERMANY;    92-GT-017 
IGTI  1992  Stage Efficiency Effects Of Vaneless Diffuser Wall Contours  J.B. Wulf, Union Carbide Industrial Gases, Tonawanda, NY, USA;    92-GT-018 
IGTI  1992  Experimental Results On A Rotatable Low Solidity Vaned Diffuser  J.M. Sorokes, J.P. Welch, Dresser-Rand Turbo Products Division, Olean, NY, USA;    92-GT-019 
IGTI  1992  Pressure Distributions In A Single And Two Versions Of A Double Volute Of A Centrifugal Pump  W. de Ojeda, R.D. Flack, University of Virginia, Charlottesville, VA, USA; S.M. Miner, U.S. Naval Academy, Annapolis, MD, USA    92-GT-020 
IGTI  1992  Solar Centaur Taurus T-6502 - The First Installation  A.L. Braun, NOVA Corporation of Alberta, Calgary, AB, CANADA;    92-GT-021 
IGTI  1992  Simplified Mathematical Representations Of Single Shaft Gas Turbines In Mechanical Drive Service  W.I. Rowen, General Electric Company, Schenectady, NY, USA;    92-GT-022 
IGTI  1992  Turbine Rebuild Effects On Gas Turbine Performance  J.D. MacLeod, National Research Council, Ottawa, ON, CANADA; B. Orbanski, Standard Aero Ltd., Winnipeg, MB, CANADA    92-GT-023 
IGTI  1992  Transient Phenomena In Compressor Stations During Surge  K. Botros, Nova Husky Research Corporation, Calgary, AB, CANADA;    92-GT-024 
IGTI  1992  Axial Inlet Conversion To A Centrifugal Compressor With Magnetic Bearings  T. Novecosky, NOVA Corporation of Alberts, Edmonton, AB, CANADA;    92-GT-025 
IGTI  1992  Foothills Decompression/Recompression Facilities - Unique Power Recovery Application In Gas Pipelines  S. Kitt, Foothills Pipelines Ltd., Calgary, AB, CANADA; B.D. Rose, Amoco Canada Petroleum Company Ltd., Calgary, AB, CANADA    92-GT-026 
IGTI  1992  Development Of A Regenerator For An Automotive Gas Turbine Engine  J. Sayama, T. Morishita, Toyota Motor Corporation, Shizuoka, JAPAN;    92-GT-027 
IGTI  1992  Compressor Fault Identification From Overall Performance Data Based On Adaptive Stage Stacking  K. Mathioudakis, A. Stamatis, National Technical University of Athens, Athens, GREECE;    92-GT-028 
IGTI  1992  Optimizing Automated Gas Turbine Fault Detection Using Statistical Pattern Recognition  E. Loukis, K. Mathioudakis, K. Papailiou, National Technical University of Athens, Athens, GREECE;    92-GT-029 
IGTI  1992  Experimental And Theoretical Analysis Of The Flow In A Centrifugal Compressor Volute  E. Ayder, R. Van den Braembussche, von Karman Institute For Fluid Dynamics, Rhode Saint Genese, BELGIUM; J.J. Brasz, Carrier Corporation, Syracuse, NY, USA    92-GT-030 
IGTI  1992  Aerodynamic Performance Of A Transonic Low Aspect Ratio Turbine Nozzle  S.H. Moustapha, Pratt & Whitney Canada, Inc., Montreal, PQ, CANADA; W.E. Carscallen, National Research Council, Ottawa, ON, CANADA; J.D. McGeachy, Queen's University, Kingston, ON, CANADA    92-GT-031 
IGTI  1992  Investigation Of Compressor Rotor Wake Structure At Peak Pressure Rise Coefficient And Effects Of Loading  J. Prato, B. Lakshminarayana, The Pennsylvania State University, University Park, PA, USA;    92-GT-032 
IGTI  1992  Pressure Fluctuation On Casing Wall Of Isolated Axial Compressor Rotors At Low Flow Rate  M. Inoue, M. Kuroumaru, Y. Ando, Kyushu University, Fukuoka, JAPAN;    92-GT-033 
IGTI  1992  Blade Loading And Shock Wave In A Transonic Circular Cascade Diffuser  H. Hayami, N. Kawaguchi, Kyushu University, Kasuga, JAPAN; M. Sawae, Nippon Mining Co., LTD., Chita, JAPAN; T. Nakamura, Toshiba Corporation, Yokohama, JAPAN    92-GT-034 
IGTI  1992  Active Control Of Complex Physical Systems: An Overview  R.J. Hansen, Office of Naval Research, Arlington, VA, USA; E.W. Hendricks, Naval Ocean Systems Center, San Diego, CA, USA    92-GT-035 
IGTI  1992  Recess Vane Passive Stall Control  M. Ziabasharhagh, A.B. McKenzie, R.L. Elder, Cranfield Inst. of Technology, Bedford, UK;    92-GT-036 
IGTI  1992  Evaluation Of Leasing Versus Purchasing Water Treatment Equipment For Cogeneration Projects  S.R. Gagnon, Process Equipment Unlimited, Londonderry, NH, USA; H.A. Guidotti, Energy Services, Inc., Farmington, CT, USA    92-GT-037 
IGTI  1992  Influence Of A Thermal Barrier Coating On The Performance Of A Turboprop Engine  J.D. MacLeod, National Research Council of Canada, Ottawa, ON, CANADA; J.C.G. Laflamme, Department of National Defence, Ottawa, ON, CANADA    92-GT-038 
IGTI  1992  Optimized High Efficiency Filter For High-Efficiency Industrial Combustion Turbines  Henry H.S. Yu, C.H. Goulding, Farr Company, El Sequndo, CA, USA;    92-GT-039 
IGTI  1992  100 MW Combined Cycle Achieves 7000 BTU/KWH Heat Rate At JFK International Airport  D.A. Kolp, S.Y. Kim, Energy Services, Inc., Farmington, CT, USA; R.Roberts, R. Roberts Consulting, Inc., The Woodlands, TX, USA    92-GT-040 
IGTI  1992  A Combustor Diffuser Of Annular Configuration Suitable For Industrial Gas Turbines  R.C. Adkins, Cranfield Institute of Technology, Cranfield, UK; A.C. Benim, P.C. Escher, J. Hellat, W.M. Koenig, ABB Turbo Systems Ltd., Baden, SWITZERLAND    92-GT-041 
IGTI  1992  Safety Aspects And Environmental Considerations For A 10 MW Cogeneration Heavy Duty Gas Turbine Burning Coke Oven Gas With 60% Hydrogen Content  J.J. Wolf, M.A. Perkavec, European Gas Turbines GMBH, Essen, GERMANY;    92-GT-042 
IGTI  1992  A Model And State-Space Controllers For An Intercooled, Regenerated (ICR) Gas Turbine Engine  J.W. Watts, T.E. Dwan, U.S. Naval Academy, Annapolis, MD, USA; R.W. Garman, David Taylor Research Center, Annapolis, MD, USA    92-GT-043 
IGTI  1992  Hot Corrosion Resistance Of Thermal Barrier Coatings  B.A. Nagaraj, A.F. Maricocchi, D.J. Wortman, General Electric Aircraft Engines, Cincinnati, OH, USA; J.S. Patton, R.L. Clarke, David Taylor Research Center, Annapolis, MD, USA    92-GT-044 
IGTI  1992  Civil Aircraft Challenges In Engine/Airframe Integration  G.L. Hamilton, H.R. Welge, McDonnell Douglas Corporation, Long Beach, CA, USA;    92-GT-045 
IGTI  1992  Development Of A Gas Turbine Generator - On Board Electric Power Source For MAGLEV Trains  T. Washizu, S. Matsuda, Toshiba Corporation, Yokohama, JAPAN; T. Morishita, Toyota Motor Corporation, Susono, JAPAN; N. Terauchi, Railway Technical Research Institute, Tokyo, JAPAN    92-GT-046 
IGTI  1992  A System Dynamics Approach To Modeling Gas Turbine Combustor Wear  B. Bagepalli, S. Dinc, I. Imam, GE Corp. Research & Development, Schenectady, NY, USA; J. Barnes, C. Slocum, GE Gas Turbine & Combined Cycle Engineering, Schenectady, NY, USA    92-GT-047 
IGTI  1992  Viscous Flows In Centrifugal Compressor Diffusers At Transonic Mach Numbers  I. Teipel, A. Wiedermann, W. Evers, University of Hannover, Hannover, GERMANY;    92-GT-048 
IGTI  1992  An Investigation On The Artificial Viscosity In The Transonic Stream Function Formulation  J.Z. Xu, J.Y. Du, H. Shen, M.C. Ge, Chinese Academy of Sciences, Beijing, CHINA;    92-GT-049 
IGTI  1992  Electromechanical Measurement Of Turbomachinery Blade Tip-To-Casing Running Clearance  A.G. Sheard, Rotodata Ltd., Derby, ENGLAND; S.R. Turner, Rolls-Royce plc, Bristol, ENGLAND    92-GT-050 
IGTI  1992  Self-Excited Vibration Of Plugs In Regulating Valves  V. Vlcek, I. Dobias, Czechoslovak Academy of Science, Prague, CZECHOSLOVAKIA;    92-GT-051 
IGTI  1992  Integration Of Condition Monitoring Technologies For the Health Monitoring Of Gas Turbines  C.B. Meher-Homji, Boyce Engineering International Inc., Houston, TX, USA; J.P. Cullen, Phillips Petroleum Company, Tananger, NORWAY    92-GT-052 
IGTI  1992  Development Of A Knowledge Based Advisory System Based On Vibration Of A Peaking Gas Turbine  R.M. Baldwin, A.J. Smalley, R.E. Harris, Southwest Research Institute, San Antonio, TX, USA; G.H. Quentin, Electric Power Research Institute, Palo Alto, CA, USA    92-GT-053 
IGTI  1992  One-Dimensional Methods For Accurate Prediction Of Off-Design Performance Behavior Of Axial Turbines  T. Schobeiri, Texas A&M University, College Station, TX, USA;    92-GT-054 
IGTI  1992  An Investigation Of Post Stall Transients And Recoverability Of Axial Compression Systems: Part I - A Simplified Method  J. Hu, G.C. Tang, H.M. Zhang, Nanjing Aeronautical Institute, Nanjing, CHINA;    92-GT-055 
IGTI  1992  An Investigation Of Post Stall Transients And Recoverability Of Axial Compression Systems: Part II - Numerical Simulations  J. Hu, G.C. Tang, H.M. Zhang, Nanjing Aeronautical Institute, Nanjing, CHINA;    92-GT-056 
IGTI  1992  Stability Of Fully Developed Rotating Stall  F.E. McCaughan, H.X. Xue, Case Western Reserve University, Cleveland, OH, USA;    92-GT-057 
IGTI  1992  A Wide-Range Axial-Flow Compressor Stage Performance Model  G.S. Bloch, Wright Patterson Air Force Base, WPAFB, OH, USA; W.F. O'Brien, Virginia Polytechnic Institute and State University, Blacksburg, VA, USA    92-GT-058 
IGTI  1992  Modified Surge In An Axial Flow Compressor  L. Pust, National Research Inst. for Machine Design, Prague, Bechovice, CZECH.;    92-GT-059 
IGTI  1992  Turbulence Evaluation Within The Secondary Flow Region Of A Turbine Cascade  D.G. Gregory-Smith, Th. Biesinger, University of Durham, Durham, UK;    92-GT-060 
IGTI  1992  Three Dimensional Transonic Flow Measurements In An Axial Turbine With Conical Walls  F. Kost, DLR, Gottingen, GERMANY;    92-GT-061 
IGTI  1992  Secondary Flows In A Transonic Cascade: Validation Of A 3-D Navier-Stokes Code  F. Bassi, Politecnico di Milano, Milano, ITALY; M. Savini, CNPM-CNR, Peschiera Borromeo, ITALY    92-GT-062 
IGTI  1992  Assessment Of A 3-D Euler Code For Subsonic Turbine Vane Flows And Study Of The Non-Radial Blade Stacking  J. Vialonga, B. Petot, SNECMA, Moissy-Cramayel, FRANCE; T. Chiappa, Ecole Des Mines De Nancy, Maisons-Alfort, FRANCE    92-GT-063 
IGTI  1992  An Investigation Of Spanwise Mixing In Multistage Axial Flow Compressors  S.-M. Li, Tsing Hua University, Beijing, CHINA; M.-Z. Chen, Beijing University of Aero. & Astro., Beijing, CHINA    92-GT-064 
IGTI  1992  Three-Dimensional Inviscid Flow Computations In A Spatial Turbopump Inducer Using A Distributed Loss Model  E.M. El Ghazzani, G. Bois, Metraflu, Ecully, FRANCE; P. Geai, Societe Europeenne de Propulsion, Vernon, FRANCE; F. Leboeuf, Ecole Centrale de Lyon, Ecully, FRANCE    92-GT-065 
IGTI  1992  The Vortex Behaviour Of The Rotating-Stall Cell Of A Centrifugal Compressor With Vaned Diffuser  Y.N. Chen, Sulzer Brothers Ltd., Winterthur, SWITZERLAND; U. Seidel, U. Haupt, M. Rautenberg, University of Hannover, Hannover, GERMANY    92-GT-066 
IGTI  1992  Flow Pattern And Heat Transfer In A Closed Rotating Annulus  D. Bohn, G.H. Dibelius, E. Deuker, R. Emunds, RWTH, Aachen, GERMANY;    92-GT-067 
IGTI  1992  Simulation Of The Secondary Air System Of Aero Engines  K.J. Kutz, T.M. Speer, MTU München GmbH, München, GERMANY;    92-GT-068 
IGTI  1992  Shroud Heat Transfer Measurements From A Rotating Cavity With An Axial Throughflow Of Air  C.A. Long, P.G. Tucker, University of Sussex, Sussex, UK;    92-GT-069 
IGTI  1992  Calculation Of Turbulent Flow For An Enclosed Rotating Cone  N.E. May, ARA Limited, Bedford, UK; J.W. Chew, Rolls-Royce Ltd, Derby, UK; P.W. James, Polytechnic South West, Plymouth, UK    92-GT-070 
IGTI  1992  Compressible Flow Pressure Losses In Wye-Junctions  N.I. Abou-Haidar, University of Leicester, Leicester, UK; S.L. Dixon, The University of Liverpool, Liverpool, UK    92-GT-071 
IGTI  1992  Aeroloads And Secondary Flows In A Transonic Mixed Flow Turbine Stage  K.R. Kirtley, T.A. Beach, Sverdrup Technology, Inc., Cleveland, OH, USA; C. Rogo, Teledyne CAE, Toledo, OH, USA    92-GT-072 
IGTI  1992  Design And Rotor Performance Of A 5:1 Mixed-Flow Supersonic Compressor  R. Monig, Rheinmetall GmbH, Dusseldorf, GERMANY; W. Elmendorf, H.E. Gallus, RWTH Aachen, Aachen, GERMANY    92-GT-073 
IGTI  1992  Aerodynamic Design Of Turbomachinery Blading In Three-Dimensional Flow: An Application To Radial Inflow Turbines  Y.L. Yang, C.S. Tan, W.R. Hawthorne, Massachusetts Institute of Technology, Cambridge, MA, USA;    92-GT-074 
IGTI  1992  Hot Streaks And Phantom Cooling In A Turbine Rotor Passage: Part 1 - Separate Effects  R.J. Roback, R.P. Dring, United Technologies Research Center, E. Hartford, CT, USA;    92-GT-075 
IGTI  1992  Hot Streaks And Phantom Cooling In A Turbine Rotor Passage: Part 2 - Combined Effects And Analytical Modelling  R.J. Roback, R.P. Dring, United Technologies Research Center, E. Hartford, CT, USA;    92-GT-076 
IGTI  1992  Extending The Fatigue Life Of Aircraft Engine Components By Hole Cold Expansion Technology  A.C. Rufin, Fatigue Technology, Inc., Seattle, WA, USA;    92-GT-077 
IGTI  1992  Fatigue Life Estimation Procedure For A Turbine Blade Under Transient Loads  N.S. Vyas, Indian Institute of Technology, Kanpur, INDIA; J.S. Rao, Indian Institute of Technology, New Delhi, INDIA    92-GT-078 
IGTI  1992  Circulator Design/Technology Evolution For Gas-Cooled Nuclear Reactors  C.F. McDonald, General Atomics, San Diego, CA, USA; D.D. Kapich, Consultant, San Diego, CA, USA; I.R. Marshall, J. Donaldson, James Howden Company, Ltd., Renfrew, Scotland, UK    92-GT-079 
IGTI  1992  An Infrared Pyrometry System For Monitoring Gas Turbine Blades: Development Of A Computer Model And Experimental Results  M. De Lucia, C. Lanfranchi, Universita delgi Studi di Firenze, Firenze, ITALY;    92-GT-080 
IGTI  1992  Effects Of Back-Pressure In A Lean Blowout Research Combustor  G.J. Sturgess, Pratt & Whitney, E. Hartford, CT, USA; S.P. Heneghan, M.D. Vangsness, D.R. Ballal, University of Dayton, Dayton, OH, USA; A.L. Lesmerises, D. Shouse, Wright Laboratories, WPAFB, OH, USA    92-GT-081 
IGTI  1992  Fault Signatures Obtained From Fault Implant Tests On An F404 Engine  R.W. Eustace, B.A. Woodyatt, G.L. Merrington, T.A. Runacres, DSTO Aeronautical Research Laboratory, Melbourne, AUSTRALIA;    92-GT-082 
IGTI  1992  The Effect Of Compressor Rotor Tip Crops On Turboshaft Engine Performance  P.C. Frith, DSTO Aeronautical Research Laboratory, Melbourne, AUSTRALIA;    92-GT-083 
IGTI  1992  Surface-Curvature-Distribution Effects On Turbine-Cascade Performance  T. Korakianitis, P. Papagiannidis, Washington University, St. Louis, MO, USA;    92-GT-084 
IGTI  1992  A Study Of Stall In A Low Hub/Tip Ratio Fan  M. Soundranayagam, National Engineering Laboratory, Glasgow, SCOTLAND; R.L. Elder, Cranfield Institute Of Technology, Bedford, ENGLAND    92-GT-085 
IGTI  1992  Investigation Of The Part-Load Performance Of Two 1.12 MW Regenerative Marine Gas Turbines  T. Korakianitis, K. Beier, Washington University, St. Louis, MO, USA;    92-GT-086 
IGTI  1992  Development Of Gas Turbine Steam-Injection Water Recovery (SIWR) System  H.B. Nguyen, A. den Otter, NOVA Corporation of Alberta, Edmonton, AB, CANADA;    92-GT-087 
IGTI  1992  Active Stabilization Of Compressor Instability And Surge In A Working Engine  J.E. Frowcs Williams, Cambridge University, Cambridge, UK; M.F.L. Harper, D.J. Allwright, Topexpress Limited, Cambridge, UK    92-GT-088 
IGTI  1992  A Survey Of Platform Machinery In The North Sea  L.E. Bakken, J.M. Overli, Statoil, Trondheim, NORWAY;    92-GT-089 
IGTI  1992  Experimental Analysis Of Transonic Flow Through The Variable Nozzle Of A Radial Inflow Turbine  H.E. Gallus, U. Lingner, RWTH Aachen, Aachen, GERMANY; I. Ispas, Atlas Copco, Koln, GERMANY    92-GT-090 
IGTI  1992  Influence Of Blade Aerodynamic Loading On Efficiency Of Radial-Inflow Turbines  T. Takamura, F. Nishiguchi, Nissan Motor Co., LTD, Yokosuka, JAPAN;    92-GT-091 
IGTI  1992  The Effects Of Blade Loading In Radial And Mixed Flow Turbines  H. Chen, M. Abidat, N.C. Baines, Imperial College, London, U.K.; M.R. Firth, Holset Engineering Company, LTD, Huddersfield, U.K.    92-GT-092 
IGTI  1992  The Design And Evaluation Of A High Pressure Ratio Radial Turbine  K.R. Pullen, N.C. Baines, Imperial College, London, U.K.; S.H. Hill, Rolls Royce plc, Herts, U.K.    92-GT-093 
IGTI  1992  Aerodynamic Design Of Pivotable Nozzle Vanes For Radial-Inflow Turbines  M. Scholch, Universitat der Bundeswehr, Hamburg, GERMANY;    92-GT-094 
IGTI  1992  Markov Fatigue In Single Crystal Airfoils  C. Annis, D.P. DeLuca, Pratt & Whitney, West Palm Beach, FL, USA;    92-GT-095 
IGTI  1992  Performance Evaluation Of Space Solar Brayton Cycle Power Systems  Z.-G. Diao, Chinese Academy of Sciences, Beijing, CHINA;    92-GT-096 
IGTI  1992  Combined Closed Cycle (C 3) Systems For Underwater Power Generation  A. Massardo, Universita di Genova, Genova, ITALY; G.M. Arnulfi, Universita di Udine, ITALY    92-GT-097 
IGTI  1992  Combined-Closed Gas Cycles For Terrestrial, Marine And Space Nuclear Power Systems  Z.P. Tilliette, DMT/SERMA, Saclay, FRANCE;    92-GT-098 
IGTI  1992  Conceptual Study On Radiator Area Reduction Of Brayton Cycle Solar Dynamic Power  Y. Tsujikawa, University of Osaka Prefecture, Sakai, JAPAN;    92-GT-099 
IGTI  1992  Condition Monitoring And Diagnostic Aspects Of Gas Turbine Transient Response  C.B. Meher-Homji, R. Bhargava, Boyce Engineering International Inc., Houston, TX, USA;    92-GT-100 
IGTI  1992  Comparisons Of Recuperator Flow Distributions Of An Intercooled-Recuperative Marine Gas Turbine  R.L. Kiang, J.L. Buyer, David Taylor Research Center, Annapolis, MD, USA; R.A. Uhlig, Applied Research Laboratory, State College, PA, USA    92-GT-101 
IGTI  1992  The LM6000 Gas Turbine As A Mechanical Drive Power Source  R.L. Casper, R.B. Spector, General Electric Company, Cincinnati, OH, USA;    92-GT-102 
IGTI  1992  A Method to Improve Operation of the Gullfaks 'A' Gas Compression System  L.E. Bakken, Statoil, Trondheim, NORWAY; T.M. Bradley, Special Analysis & Simulation Tech. Ltd., Brentford, UK    92-GT-103 
IGTI  1992  Applications Using Dry Gas Seals To Control Axial Shaft Loads In Centrifugal Compressors  C.C. Bear, S.W. Gibson, NOVA Corporation, Calgary, CANADA;    92-GT-104 
IGTI  1992  Carbon Monoxide Emissons From Gas Turbines As Influenced By Ambient Temperature And Turbine Load  W.S.Y. Hung, Solar Turbines Incorporated, San Diego, CA, USA;    92-GT-105 
IGTI  1992  Studies Of Jet Fuel Thermal Stability In A Flowing System  S.P. Heneghan, C.R. Martel, T.F. Williams, D.R. Ballal, University of Dayton, Dayton, OH, USA;    92-GT-106 
IGTI  1992  Liquid Sheet Disintegration And Atomization Process On A Simplified Airblast Atomizer  G. Lavergne, P. Trichet, P. Hebrard, Y. Biscos, CERT / ONERA / DERMES, Toulouse, FRANCE;    92-GT-107 
IGTI  1992  Modification Of Combustor Stoichiometry Distribution For Reduced NOx Emission From Aircraft Engines  G.J. Sturgess, R. McKinney, S. Morford, Pratt & Whitney, E. Hartford, CT, USA;    92-GT-108 
IGTI  1992  Low NOx Combustor For Automotive Ceramic Gas Turbine (II) -- Reliability Assurance  H. Kumakura, M. Sasaki, D. Suzuki, Nissan Motor Co., Ltd., Kanagawa, JAPAN;    92-GT-109 
IGTI  1992  Emissions Reduction By Varying The Swirler Airflow Split In Advanced Gas Turbine Combustors  G.J. Micklow, S. Roychoudhury, University of Florida, Gainsville, FL, USA; H.L. Nguyen, NASA Lewis Research Center, Cleveland, OH, USA; M.C. Cline, Los Alamos Natonal Laboratory, Los Alamos, NM, USA    92-GT-110 
IGTI  1992  Multi-Jet Annulus/Core-Flow Mixing - Experiments And Calculations  J.J. McGuirk, Loughborough University, Leics., U.K.; S.J. Baker, Imperial College, London, U.K.    92-GT-111 
IGTI  1992  Development Of A Liquid-Fueled, Lean-Premixed Gas Turbine Combustor  L.H. Cowell, K.O. Smith, Solar Turbines Incorporated, San Diego, CA, USA;    92-GT-112 
IGTI  1992  Particle Diagnostics And Turbulence Measurements In A Confined Isothermal Liquid Spray  A. Brena de la Rosa, S.V. Sankar, G. Wang, W.D. Bachalo, Aerometrics, Inc., Sunnyvale, CA, USA;    92-GT-113 
IGTI  1992  Influence Of Flow Conditions On Deposits From Heated Hydrocarbon Fuels  J.S. Chin, A.H. Lefebvre, Purdue University, W. Lafayette, IN, USA;    92-GT-114 
IGTI  1992  NOx Sensitivities For Gas Turbine Engines Operated On Lean-Premixed Combustion And Conventional Diffusion Flames  D. Nicol, P.C. Malte, J. Lai, N.N. Marinov, D.T. Pratt, University of Washington, Seattle, WA, USA; R.A. Corr, General Electric Company, Schenectady, NY, USA    92-GT-115 
IGTI  1992  Engine Testing Of A Prototype Low NOx Gas Turbine Combustor  K.O. Smith, Solar Turbines Incorporated, San Diego, CA, USA;    92-GT-116 
IGTI  1992  A Liquid-Pool Simulation On Droplet Combustion In A Swirl Flow  T.-H. Lin, S.-S. Hou, National Cheng Kung University, Taiwan, CHINA;    92-GT-117 
IGTI  1992  Experimental And Computational Investigation Of Flow In Catalytic Monolith Channels  G.C. Wilson, M.F. Bardon, Royal Military College of Canada, Kingston, CANADA; J.J. Witton, Cranfield Institute of Technology, Cranfield, UK    92-GT-118 
IGTI  1992  Ignition And Exhaust Emission Characteristics Of Spray Combustion In A Pre-Chamber Type Vortex Combustor  Y. Ohkubo, Y. Nomura, Y. Idota, Toyota Central R&D Labs, Inc., Nagadute, Aichi, JAPAN; Y. Gunji, Toyota Motor Corporation, Susono, Shizuoka, JAPAN    92-GT-119 
IGTI  1992  Emissions And Stability Characteristics Of Flameholders For Lean-Premixed Combustion  J.A. Lovett, N. Abuaf, General Electric Company, Schenectady, NY, USA;    92-GT-120 
IGTI  1992  Effect Of Initial Fuel Distribution And Subsequent Mixing On Emissions From Lean, Premixed Flames  J.R. Maughan, R.E. Warren, A.K. Tolpadi, T.P. Roloff, General Electric Company, Schenectady, NY, USA;    92-GT-121 
IGTI  1992  Application Of A Sulphur-Doped Alkane System To The Study Of Thermal Oxidation Of Jet Fuels  E.G. Jones, W.J. Balster, Systems Research Laboratories, Inc., Dayton, OH, USA;    92-GT-122 
IGTI  1992  Investigation Of Combustion Structure Inside Low NOx Combustors For A 1500 C-Class Gas Turbine  H. Matsuzaki, Tohoku Electric Power Co., Inc., Miyagi, JAPAN; I. Fukue, S. Mandai, M. Inada, S. Tanimura, Mitsubishi Heavy Industries, Hyogo, JAPAN    92-GT-123 
IGTI  1992  Structure Of A Hollow-Cone Spray With And Without Combustion  B. Chehroudi, M. Ghaffarpour, UIC Combustion Laboratory, Chicago, IL, USA;    92-GT-124 
IGTI  1992  The Combined Closed Form - Perturbation Approach To The Analysis Of Mistuned Bladed Disks  M.P. Mignolet, C.-C. Lin, Arizona State University, Tempe, AZ, USA;    92-GT-125 
IGTI  1992  The Effect Of Inlet Swirl On The Rotordynamic Shroud Forces In A Centrifugal Pump  A. Guinzburg, E.P.F.L., Lausanne, SWITZERLAND; C.E. Brennen, A. Acosta, T.K. Caughey, California Institute of Technology, Pasadena, CA, USA    92-GT-126 
IGTI  1992  Analysis Of Steady And Unsteady Turbine Cascade Flows By A Locally Implicit Hybrid Algorithm  C.J. Hwang, J.L. Liu, National Cheng Kung University, Taiwan, CHINA;    92-GT-127 
IGTI  1992  An Inviscid-Viscous Interaction Approach To The Calculation Of Dynamic Stall Initiation On Airfoils  T. Cebeci, H.M. Jang, H.H. Chen, California State University, Long Beach, CA, USA; M.F. Platzer, Naval Postgraduate School, Monterey, CA, USA    92-GT-128 
IGTI  1992  Three-Dimensional Gas Turbine Combustor Emissions Modeling  N.K. Rizk, H.C. Mongia, General Motors Corporation, Indianapolis, IN, USA;    92-GT-129 
IGTI  1992  Semianalytical Correlations For NOx, CO, And UHC Emissions  N.K. Rizk, H.C. Mongia, General Motors Corporation, Indianapolis, IN, USA;    92-GT-130 
IGTI  1992  Effects Of Variable Liquid Properties On Multicomponent Droplet Vaporization  R. Kneer, B. Noll, S. Wittig, Universitat Karlsruhe, Karlsruhe, GERMANY; M. Schneider, Arizona State University, Tempe, AZ, USA    92-GT-131 
IGTI  1992  Innovative High Temperature Aircraft Engine Fuel Nozzle Design  R.W. Stickles, W.J. Dodds, GE Aircraft Engines, Cincinnati, OH, USA; T.R. Koblish, J. Sager, Fuel Systems Textron, Zeeland, MI, USA; S. Clouser, Naval Air Propulsion Center, Trenton, NJ, USA    92-GT-132 
IGTI  1992  Evaluation Of Low NOx Combustor Concepts For Aeroderivative Gas Turbine Engines  J.B. McVey, F.C. Padget, T.J. Rosfjord, United Technologies Research Center, E. Hartford, CT, USA; A.S. Hu, A.A. Peracchio, B. Schlein, D.R. Tegel, Pratt & Whitney, E. Hartford, CT, USA    92-GT-133 
IGTI  1992  Coherent Anti-Stokes Raman Scattering (CARS) Thermometry In A Model Gas Turbine Can Combustor  J.Y. Zhu, T. Tsuruda, W.A. Sowa, G.S. Samuelsen, University of California, Irvine, CA, USA;    92-GT-134 
IGTI  1992  The Combustion Of Droplets Within Gas Turbine Combustors Some Recent Observations On Combustion Efficiency  J. Odgers, D. Kretschmer, Laval University, Quebec, CANADA; G.F. Pearce, ARL, Melbourne, AUSTRALIA    92-GT-135 
IGTI  1992  Calculation Of Three-Dimensional Unsteady Flows In Turbomachinery Using The Linearized Harmonic Euler Equations  K.C. Hall, C.B. Lorence, Duke University, Durham, NC, USA;    92-GT-136 
IGTI  1992  Experimental And Theoretical Investigation Of A Research Atomizer/Combustion Chamber Configuration  C. Hassa, E. Blumcke, M. Brandt, H. Eickhoff, DLR, Koln, GERMANY;    92-GT-137 
IGTI  1992  Three Component LDV Velocity Measurements In A Can Type Research Combustor For CFD Validation, Part 1: Isothermal  S.A. Ahmed, A.S. Nejad, Wright Laboratory, WPAFB, OH, USA; A. Rose, Rolls-Royce Inc., Dayton, OH, USA    92-GT-138 
IGTI  1992  Achieving Manufacturing Excellence For Gas Turbine Components Through Focused Implementation Of Technology  C. Hayner, Pratt & Whitney, Southington, CT, USA;    92-GT-139 
IGTI  1992  Evaluation Of Simple Aluminide And Platinum Modified Aluminide Coatings On High Pressure Turbine Blades After Factory Engine Testing - Round II  J.A. Conner, GE Aircraft Engines, Cincinnati, OH, USA;    92-GT-140 
IGTI  1992  Low Leakage Fiber Metal Seals  G.P. Jarrabet, L. Lu, Technetics Corporation, Deland, FL, USA;    92-GT-141 
IGTI  1992  Corrosion Resistance Of Alloy 617 In Simulated Gas Turbine Environments  P. Ganesan, G.D. Smith, D.H. Yates, Inco Alloys International, Inc., Huntington, WV, USA;    92-GT-142 
IGTI  1992  A Digital Fuel Control System For Marine Propulsion Applications  T. Burgess, Woodward Governor Company, Ft. Collins, CO, USA;    92-GT-143 
IGTI  1992  Phasing The Construction Of An IGCC Plant For Fuel Flexibility  P.J. Dechamps, Ph. Mathieu, University of Liege, Liege, BELGIUM;    92-GT-144 
IGTI  1992  Second-Law Analysis Of A Compressed Air Energy Storage (CAES) System  D. Weiner, I. Shnaid, Israel Electric Corp. Ltd., Haifa, ISRAEL;    92-GT-145 
IGTI  1992  Modified Combined Cycle With Pressure Fluidized Bed Combustion Boiler  J. Dzierzgowski, S. Sobkowski, Technical University of Gdansk, Gdansk, POLAND;    92-GT-146 
IGTI  1992  An Update On The Development Of The T407/GLC38 Modern Technology Gas Turbine Engine  M.J. Zoccoli, D.P. Rusterholz, Textron Lycoming, Stratford, CT, USA;    92-GT-147 
IGTI  1992  Blade Excitation By Circumferentially Asymmetric Rotating Stall In Centrifugal Compressors  D. Jin, U. Haupt, H. Hasemann, M. Rautenberg, University of Hannover, Hannover, GERMANY;    92-GT-148 
IGTI  1992  Excitation Of Blade Vibration Due To Surge Of Centrifugal Compressors  D. Jin, U. Haupt, H. Hasemann, M. Rautenberg, University of Hannover, Hannover, GERMANY;    92-GT-149 
IGTI  1992  Sound Propagation Calculation Over Larger Distances On A Standardized Basis According To The German VDI- Regulations No. 2714  M. Schneider, Werner Genest & Partner Consulting Engrs., Ludwigshafen, GERMANY;    92-GT-150 
IGTI  1992  Calculations On The Time-Dependent Potential Flow In A Centrifugal Pump  R. Badie, J.B. Jonker, T.G. van Essen, University of Twente, Enschede, NETHERLANDS;    92-GT-151 
IGTI  1992  Unsteady Pressure Measurements In A Rotating Centrifugal Impeller  G. Roth, University of Stuttgart, Stuttgart, GERMANY;    92-GT-152 
IGTI  1992  Profile Losses Of An Annular Turbine Cascade In Unsteady Periodic Flow  M. Lisal, P. Soch, J. Vratny, Czech Technical University, Prague, CZECHOSLOVAKIA;    92-GT-153 
IGTI  1992  Comparison Between Experiment And Prediction For A Subsonic Turbulent Separated Boundary Layer  D. Bohn, G.H. Dibelius, Z. Sucharski, RWTH Aachen, Aachen, GERMANY;    92-GT-154 
IGTI  1992  Boundary Layer Effects On The Transonic Flow In A Straight Turbine Cascade  M. Stastny, P. Safarik, SKODA, Plezn, CZECHOSLOVAKIA;    92-GT-155 
IGTI  1992  Unsteady Pressure Measurements On The Rotor Of A Model Turbine Stage In A Transient Flow Facility  A.J. Dietz, Royal Australian Air Force, Edinburgh, S. Australia; R.W. Ainsworth, Oxford University, Oxford, ENGLAND    92-GT-156 
IGTI  1992  Techniques For Aerodynamic Loss Measurement Of Transonic Turbine Cascades With Trailing-edge Region Coolant Ejection  D.J. Mee, University of Queensland, Queensland, AUSTRALIA;    92-GT-157 
IGTI  1992  Transonic Flow Through Turbine Cascades With Nonuniform Pitch  R. Kurz, Deutsche Babcock-Borsig, Berlin, GERMANY;    92-GT-158 
IGTI  1992  Turbine Blade Vibration Monitoring System  T. Kawashima, H. Iinuma, T. Wakatsuki, N. Minagawa, Ishikawajima-Harima Heavy Industries, Tokyo, JAPAN;    92-GT-159 
IGTI  1992  Rim Seal Experiments And Analysis Of A Rotor-Stator System With Nonaxisymmetric Main Flow  K. Hamabe, K. Ishida, Kawasaki Heavy Industries, Ltd., Adashi, JAPAN;    92-GT-160 
IGTI  1992  Non-Steady Flow Measurements Inside A Hydrodynamic Torque Converter By Hot-Film Anemometry  V. Browarzik, K.G. Grahl, Ruhr-Universitat Bochum, Bochum, GERMANY;    92-GT-161 
IGTI  1992  Viscous Interaction Upstream And Downstream Of A Turbine Stator Cascade With A Periodic Wake Field  V.E. McFarland, W.G. Tiederman, Purdue University, W. Lafayette, IN, USA;    92-GT-162 
IGTI  1992  Optimization Of A Multistage Axial Compressor. Stochastic Approach.  I.N. Egorov, Air Force Engineering Academy, Moscow, USSR;    92-GT-163 
IGTI  1992  Vibration Of A Rigid Shaft Supported By Radial Ball Bearings With Several Defects  J.M. Franco, N. Akturk, R. Gohar, Imperial College, London, UK;    92-GT-164 
IGTI  1992  Effect Of Tangential Torque On The Stability Of Rotors Supported By Hydrodynamic Bearings  D.-C. Han, Seoul National University, Seoul, KOREA;    92-GT-165 
IGTI  1992  The Dynamic Characteristics Of A High Pressure Turbine Stage In A Transient Wind Tunnel  A.G. Sheard, Rotadata Ltd., Derby, ENGLAND; A.J. Dietz, Royal Australian Air Force, AUSTRALIA; R.W. Ainsworth, University of Oxford, Oxford, ENGLAND    92-GT-166 
IGTI  1992  Computational Techniques For Probabilistic Analysis Of Turbomachinery  H.R. Millwater, A.J. Smalley, Y.-T. Wu, T.Y. Torng, B.F. Evans, Southwest Research Institute, San Antonio, TX, USA;    92-GT-167 
IGTI  1992  Stability Of A Pretwisted Blade With Nonconstant Rotating Speed  S.M. Yang, S.M. Tsao, National Cheng Kung University, Taiwan, CHINA;    92-GT-168 
IGTI  1992  Three-Dimensional Flow Phenomena In A Transonic, High-Through-Flow, Axial-Flow Compressor Stage  W.W. Copenhaver, S.L. Puterbaugh, Wright Laboratory, Wright Patterson AFB, OH, USA; C. Hah, NASA Lewis Research Center, Cleveland, OH, USA    92-GT-169 
IGTI  1992  Coupled 3-D Aeroelastic Stability Analysis Of Bladed Disks  G.A. Gerolymos, Universite Pierre & Marie Curie, Paris, FRANCE;    92-GT-170 
IGTI  1992  Advances In The Numerical Integration Of The 3-D Euler Equations In Vibrating Cascades  G.A. Gerolymos, Universite Pierre & Marie Curie, Paris, FRANCE;    92-GT-171 
IGTI  1992  An Analysis System For Blade Forced Response  H.D. Chiang, R.E. Kielb, GE Aircraft Engines, Cincinnati, OH, USA;    92-GT-172 
IGTI  1992  Numerical Solutions For Unsteady Subsonic Vortical Flows Around Loaded Cascades  J. Fang, H.M. Atassi, University of Notre Dame, IN, USA;    92-GT-173 
IGTI  1992  Forcing Function Effects On Unsteady Aerodynamic Gust Response Part 1: Forcing Functions  G.H. Henderson, Cummins Engine Company, Columbus, IN, USA; S. Fleeter, Purdue University, W. Lafayette, IN, USA    92-GT-174 
IGTI  1992  Forcing Function Effects On Unsteady Aerodynamic Gust Response Part 2: Low Solidity Airfoil Row Response  G.H. Henderson, Cummins Engine Company, Columbus, IN, USA; S. Fleeter, Purdue University, W. Lafayette, IN, USA    92-GT-175 
IGTI  1992  Applications Of Sweep Frequency Rotating Force Perturbation Methodology In Rotating Machinery For Dynamic Stiffness Identification  A. Muszynska, D.E. Bently, W.D. Franklin, J.W. Grant, P. Goldman, Bently Rotor Dynamics Research Corporation, Minden, NV, USA;    92-GT-176 
IGTI  1992  A Study Of The Influence Of Bearing Clearance On Lateral Coupled Shaft/Disk Rotordynamics  G.T. Flowers, F.S. Wu, Auburn University, Auburn, AL, USA;    92-GT-177 
IGTI  1992  Effect Of Trailing-Edge Ejection On Local Heat (Mass) Transfer In Pin Fin Cooling Channels In Turbine Blades  R.D. McMillin, S.C. Lau, Texas A&M University, College Station, TX, USA;    92-GT-178 
IGTI  1992  Tools For Diagnosing Case Deflections And Alignment On A Power Utility Combustion Turbine  H.R. Simmons, A.J. Smalley, Southwest Research Institute, San Antonio, TX, USA; R.W. Fischmuth, Electric Power Research Institute, Palo Alto, CA, USA; G. Lapini, CISE S.P.A., Segrate, ITALY; G. Robinson, Westinghouse Electric Corporation, Orlando, FL, USA    92-GT-179 
IGTI  1992  Behaviors Of The Laterally Injected Jet In Film Cooling: Measurements Of Surface Temperature And Velocity/Temperature Field Within The Jet  S. Honami, T. Shizawa, Science University of Tokyo, Tokyo, JAPAN; A. Uchiyama, Mitsubishi Heavy Industries Ltd., Hyogo, JAPAN    92-GT-180 
IGTI  1992  Experimental Study On The Flow Characteristics Of Streamwise Inclined Jets In Crossflow On Flat Plate  S.W. Lee, J.S. Lee, S.T. Ro, Seoul National University, Seoul, KOREA;    92-GT-181 
IGTI  1992  Evaluation Of Approaches To Active Compressor Surge Stabilization  J.S. Simon, L. Valavani, A.H. Epstein, E.M. Greitzer, Massachusetts Institute of Technology, Cambridge, MA, USA;    92-GT-182 
IGTI  1992  Aerodesign And Performance Analysis Of A Radial Transonic Impeller For A 9:1 Pressure Ratio Compressor  S. Colantuoni, A. Colella, Alfa Romeo Avio S.p.A., Napoli, ITALY;    92-GT-183 
IGTI  1992  Incidence Angle And Pitch-Chord Effects On Secondary Flows Downstream Of A Turbine Cascade  A. Perdichizzi, V. Dossena, C.N.P.M., Milano, ITALY;    92-GT-184 
IGTI  1992  Low Aspect Ratio Transonic Rotors: Part 1 - Baseline Design And Performance  A.R. Wadia, GE Aircraft Engines, Cincinnati, OH, USA; C.H. Law, Wright Laboratory, Wright Patterson AFB, OH, USA    92-GT-185 
IGTI  1992  Low Aspect Ratio Transonic Rotors: Part 2 - Influence Of Location Of Maximum Thickness On Transonic Compressor Performance  A.R. Wadia, GE Aircraft Engines, Cincinnati, OH, USA; C.H. Law, Wright Laboratory, Wright Patterson AFB, OH, USA    92-GT-186 
IGTI  1992  Heat Transfer And Turbulence In A Turbulated Blade Cooling Circuit  N. Abuaf, General Electric Company, Schenectady, NY, USA; D.M. Kercher, GE Aircraft Engines, Lynn, MA, USA    92-GT-187 
IGTI  1992  Influence Of Surface Heating Condition On Local Heat Transfer In A Rotating Square Channel With Smooth Walls And Radial Outward Flow  J.C. Han, Y.M. Zhang, Texas A&M University, College Station, TX, USA; C.P. Lee, General Electric Company, Cincinnati, OH, USA    92-GT-188 
IGTI  1992  Experimental Heat Transfer Investigation Of Stationary And Orthogonally Rotating Asymmetric And Symmetric Heated Smooth And Turbulated Channels  H.A. El-Husayni, M.E. Taslim, Northeastern University, Boston, MA, USA; D.M. Kercher, GE Aircraft Engines, Lynn, MA, USA    92-GT-189 
IGTI  1992  Heat Transfer In Serpentine Flow Passages With Rotation  S. Mochizuki, J. Takamura, Tokyo University of Agriculture & Technology, Tokyo, JAPAN; S. Yamawaki, Ishikawajima-Harima Heavy Industries, Tokyo, JAPAN; W.-J. Yang, University of Michigan, Ann Arbor, MI, USA    92-GT-190 
IGTI  1992  Heat Transfer In Rotating Serpentine Passages With Trips Skewed To The Flow  B.V. Johnson, J.H. Wagner, United Technologies Research Center, E. Hartford, CT, USA; G.D. Steuber, Pratt & Whitney, E. Hartford, CT, USA; F.C. Yeh, NASA Lewis Research Center, Cleveland, OH, USA    92-GT-191 
IGTI  1992  Discharge Coefficients Of Holes Angled To The Flow Direction  N. Hay, S.E. Henshall, A. Manning, University of Nottingham, Nottingham, UK;    92-GT-192 
IGTI  1992  The Solution-Adaptive Numerical Simulation Of The 3D Viscous Flow In The Serpentine Coolant Passage Of A Radial Inflow Turbine Blade  W.N. Dawes, Whittle Laboratory, Cambridge, UK;    92-GT-193 
IGTI  1992  Time-Averaged Heat Transfer And Pressure Measurements And Comparison With Prediction For A Two-Stage Turbine  M.G. Dunn, J. Kim, Calspan-UB Research Center, Buffalo, NY, USA; K.C. Civinskas, R.J. Boyle, NASA Lewis Research Center, Cleveland, OH, USA    92-GT-194 
IGTI  1992  An Experimental Study Of Heat Transfer In A Large-Scale Turbine Rotor Passage  M.F. Blair, United Technologies Research Center, E. Hartford, CT, USA;    92-GT-195 
IGTI  1992  Wake-Induced Unsteady Stagnation-Region Heat-Transfer Measurements  P.J. Magari, Osney Laboratory, Oxford, UK; J.E. LaGraff, Syracuse University, Syracuse, NY, USA    92-GT-196 
IGTI  1992  The Effect Of A Turbulent Wake On The Stagnation Point Part II: Heat Transfer Results  A.J. Hanford, D.E. Wilson, University of Texas, Austin, TX, USA;    92-GT-197 
IGTI  1992  Heat Transfer On A Flat Surface Under A Region Of Turbulent Separation  R.B. Rivir, Wright Laboratories, WPAFB, OH, USA; J.P. Johnston, J.K. Eaton, Stanford University, Stanford, CA, USA    92-GT-198 
IGTI  1992  Interactions Between Embedded Vortices And Injectant From Film Cooling Holes With Compound Angle Orientations In A Turbulent Boundary Layer  P.M. Ligrani, S.W. Mitchell, Naval Postgraduate School, Monterey, CA, USA;    92-GT-199 
IGTI  1992  Tip Clearance Effect On Heat Transfer And Leakage Flows On The Shroud-Wall Surface In An Axial Flow Turbine  M. Kumada, S. Iwata, Gifu University, Gifu, JAPAN; M. Obata, Isshikawajima-Harima Heavy Industries Co., Ltd., Tokyo, JAPAN; O. Watanabe, Toyo Denki Co., Ltd., Kasugai-city, JAPAN    92-GT-200 
IGTI  1992  An Experimental Study Of Film Cooling In A Rotating Transonic Turbine  R.S. Abhari, Textron Lycoming, Stratford, CT, USA; A.H. Epstein, Massachusetts Institute of Technology, Cambridge, MA, USA    92-GT-201 
IGTI  1992  Comparison Of Spectrometric Techniques For The Analysis Of Liquid Gas Turbine Fuels  M. Lukas, Spectro Incorporated, Littleton, MA, USA;    92-GT-202 
IGTI  1992  The Evolution Of Thermal Barrier Coatings In Gas Turbine Engine Applications  S.M. Meier, D.K. Gupta, Pratt & Whitney, E. Hartford, CT, USA;    92-GT-203 
IGTI  1992  Integration Of Turbo Expander And Turbo Ramjet Engines In Hypersonic Vehicles  B. Zellner, W. Sterr, O. Herrmann, MBB GmbH, München, GERMANY;    92-GT-204 
IGTI  1992  Hypersonic Flow Separation In Shock Wave Boundary Layer Interactions  A. Hamed, University of Cincinnati, Cincinnati, OH, USA; A. Kumar, NASA Langley Research Center, Hampton, VA, USA    92-GT-205 
IGTI  1992  Numerical Simulation Of The Flow Field Around Supersonic Air-Intakes  O. Penanhoat, SNECMA, Moissy-Cramayel, FRANCE; G. Freskos, CERFACS, Toulouse, FRANCE    92-GT-206 
IGTI  1992  Scaling Of The Two-Phase Flow Downstream Of A Gas Turbine Combustor Swirl Cup: Mean Quantities  H.Y. Wang, V.G. McDonell, W.A. Sowa, G.S. Samuelsen, University of California, Irvine, CA, USA;    92-GT-207 
IGTI  1992  Reliability Measurements For Gas Turbine Warranty Situations  T.E. Ekstrom, GE Power Generation, Schenectady, NY, USA;    92-GT-208 
IGTI  1992  A Fully Three-Dimensional Inverse Method For Turbomachinery Blading In Transonic Flows  T.Q. Dang, Syracuse University, Syracuse, NY, USA;    92-GT-209 
IGTI  1992  Calculation Of Three-Dimensional Boundary Layers On Rotor Blades Using Integral Methods  M.T. Karimipanah, E. Olsson, Chalmers University of Technology, Goteborg, SWEDEN;    92-GT-210 
IGTI  1992  Measurement Of The Three-Dimensional Tip Region Flowfield In An Axial Compressor  R.C. Stauter, United Technologies Research Center, E. Hartford, CT, USA;    92-GT-211 
IGTI  1992  Relative Flow And Turbulence Measurements Downstream Of A Backward Centrifugal Impeller  M. Ubaldi, R. Zunino, A. Cattanei, Universita di Genova, Genova, ITALY;    92-GT-212 
IGTI  1992  Experimental And Computational Investigation Of The NASA Low-Speed Centrifugal Compressor Flow Field  M.D. Hathaway, R.M. Chriss, J.R. Wood, A.J. Strazisar, NASA Lewis Research Center, Cleveland, OH, USA;    92-GT-213 
IGTI  1992  The Measurement And Prediction Of The Tip Clearance Flow In Linear Turbine Cascades  F.J.G. Heyes, H.P. Hodson, Whittle Laboratory, Cambridge, ENGLAND;    92-GT-214 
IGTI  1992  Experimental Study On The Three Dimensional Flow Within A Compressor Cascade With Tip Clearance: Part I -- Velocity And Pressure Fields  S. Kang, Ch. Hirsch, Vrije Universiteit Brussel, Brussel, BELGIUM;    92-GT-215 
IGTI  1992  An Investigation Of Factors Influencing The Calibration Of 5-Hole Probes For 3-D Flow Measurements  R.G. Dominy, University of Durham, Durham, ENGLAND; H.P. Hodson, Cambridge University, Cambridge, ENGLAND    92-GT-216 
IGTI  1992  On The Conservation Of Rothalpy In Turbomachines  F.A. Lyman, Syracuse University, Syracuse, NY, USA;    92-GT-217 
IGTI  1992  Investigations On A Radial Compressor Tandem-Rotor Stage With Adjustable Geometry  B. Josuhn-Kadner, Ruhr Universitat Bochum, Bochum, GERMANY; B. Hoffmann, DLR, Koln, GERMANY    92-GT-218 
IGTI  1992  Deposition Of Volcanic Materials In The Hot Sections Of Two Gas Turbine Engines  J. Kim, M.G. Dunn, A.J. Baran, Calspan Corporation, Buffalo, NY, USA; D.P. Wade, E.L. Tremba, Defense Nuclear Agency, Alexandria, VA, USA    92-GT-219 
IGTI  1992  Performance And Emission Levels In Gas Turbine Plants  F. Bozza, R. Tuccillo, University of Naples, Naples, ITALY; G. Fontana, University of Cassino, Cassino, ITALY    92-GT-220 
IGTI  1992  What Affects The Cost Of Hot Gas Filter Stations?  J.F. Zievers, P. Eggerstedt, Industrial Filter & Pump Mfg. Co., Cicero, IL, USA; E.C. Zievers, Universal Porosics, Inc., LaGrange, IL, USA; D. Nicolai, SETEC GmbH, Bietigheim, GERMANY    92-GT-221 
IGTI  1992  A Binary Gas Composition Sensor To Measure Impermeable Wall Concentration In Film Cooling Experiments  R. Seffal, S.G. Schwarz, S.J. Walker, Turlane University, New Orleans, LA, USA;    92-GT-222 
IGTI  1992  The Quasi-Three Dimensional Design Method For Steam Turbines With Curvilinear Leaned And Twisted Stator Blades  W. Zhongqi, L. Fengjun, Harbin Institute of Technology, Harbin, CHINA;    92-GT-223 
IGTI  1992  The Optimum Value Of The Nozzle Outlet Angle Of Turbine Stages  K. Kosowski, Technical University of Gdansk, Gdansk, POLAND;    92-GT-224 
IGTI  1992  Experimental Verification Of The Improvements Achieved By A New LP-Blade Design In A Steam Turbine  H. Stetter, G. Eyb, C. Zimmerman, University of Stuttgart, Stuttgart, GERMANY; H.G. Hosenfeld, Siemens AG/KWU, GERMANY    92-GT-225 
IGTI  1992  Analysis Of Normal Mode Localization In Mistuned Bladed-Disc Assembly With Disc Coupling  Y.-Q. Zhang, W.-L. Wang, Fudan University, Shanghai, CHINA;    92-GT-226 
IGTI  1992  Flutter Of Grouped Turbine Blades  D.S. Whitehead, Consultant, Wilts, ENGLAND; D.H. Evans, Westinghouse Electric Corporation, Orlando, FL, USA    92-GT-227 
IGTI  1992  Advanced Ducted Engines: Impact Of Unsteady Aerodynamics On Fan Vibration Properties  A.H. Klose, MTU, Munich, GERMANY;    92-GT-228 
IGTI  1992  Flexible Manufacturing Of Aircraft Engine Parts  O.M. Hassan, D.M. Jenkins, GE Aircraft Engines, Lynn, MA, USA;    92-GT-229 
IGTI  1992  Digital Control Retrofit Of An Industrial Gas Turbine  A. Metzger, T. Kness, Woodward Governor Co., Ft. Collins, CO, USA;    92-GT-230 
IGTI  1992  On Modeling Centrifugal Compressors For Robust Control Design  K.M. Murphy, D. Marchio, Ecole des Mines de Paris, Paris, FRANCE; P. Kalatta, R. Fischl, Drexel University, Philadelphia, PA, USA    92-GT-231 
IGTI  1992  Embedded Microprocessor Digital Control For Vehicular Turbine Management System  M. Kundra, Textron Lycoming, Stratford, CT, USA; J. Bluish, Allied Signal Aerospace Company, South Bend, IN, USA    92-GT-232 
IGTI  1992  The Quantitative Visualisation Of The Flow In A 1/10th Scale Model Thrust Reverser At The Aircraft Research Association, Bedford  P. Bryanston-Cross, Warwick University, Coventry, UK; R.S. Sale, Aircraft Research Association Ltd, Bedford, ENGLAND    92-GT-233 
IGTI  1992  Design And Test Of A Low-NOx Advanced Rich-Lean Combustor For LBG Fueled 1300 C-Class Gas Turbine  T. Nakata, M. Sato, T. Ninomiya, Central Research Institute of Electric Power Industry, Yokosuka, JAPAN; T. Yoshine, M. Yamada, Toshiba Corporation, Yokohama, JAPAN    92-GT-234 
IGTI  1992  Design Features Influencing The Distribution Of Fuel Within The Spray From An Air Blast Fuel Injector  F.W. Stringer, A.N. Irwin, AIT Limited, Lancashire, ENGLAND;    92-GT-235 
IGTI  1992  Operating Experience And Site Performance Testing Of The CW251B12 Gas Turbine Engine  I.S. Diakunchak, Westinghouse Canada, Inc., Hamilton, ON, CANADA;    92-GT-236 
IGTI  1992  501F Development Update  D.T. Entenmann, K.G. Hultgren, J.P. Smed, Westinghouse Electic Corporation, Orlando, Fl, USA; K. Aoyama, K. Tsukagoshi, S. Umemura, Mitsubishi Heavy Ind, Ltd, Takasago, JAPAN    92-GT-237 
IGTI  1992  Application Of Digital Video Interactive Technology For Operation And Maintenance Of Industrial Gas Turbines  K. Golas, S. Mutter, A.J. Smalley, Southwest Research Institute, San Antonio, TX, USA; G. Quentin, Electric Power Research Institute, San Jose, CA, USA    92-GT-238 
IGTI  1992  Turbulent Flow And Heat Transfer In Gas Turbine Blade Cooling Passages  F.J. Cunha, General Electric Company, Schenectady, NY, USA;    92-GT-239 
IGTI  1992  New Advanced Cooling Technology And Material Of The 1500 C Class Gas Turbine  H. Matsuzaki, K. Shimomura, Tohoku Electric Company, Inc., Sendai, JAPAN; Y. Fukuyama, T. Araki, J. Ishii, M. Yamamoto, S. Shibuya, I. Okuhara, Toshiba Corporation, Yokohama, JAPAN    92-GT-240 
IGTI  1992  Internal Cooling Passage Heat Transfer Near The Entrance To A Film Cooling Hole: Experimental And Computational Results  A.R. Byerley, United States Air Force Academy, Colorado Springs, CO, USA; T.V. Jones, P.T. Ireland, Oxford University, Oxford, UK    92-GT-241 
IGTI  1992  Pin-Fin Heat Transfer: Contribution Of The Wall And The Pin To The Overall Heat Transfer  A.M. Al Dabagh, G.E. Andrews, University of Leeds, Leeds, UK;    92-GT-242 
IGTI  1992  Heat Transfer And Aerodynamics Of A High Rim Speed Turbine Nozzle Guide Vane With Profiled End Walls  K.S. Chana, Defense Research Agency, Hampshire, UK;    92-GT-243 
IGTI  1992  Measurements Of The Effect Of Free-Stream Turbulence Length Scale On Heat Transfer  R.W. Moss, M.L.G. Oldfield, University of Oxford, Oxford, UK;    92-GT-244 
IGTI  1992  An Improved Boundary Layer Transition Correlation  A. Fasihfar, M.W. Johnson, University of Liverpool, Liverpool, UK;    92-GT-245 
IGTI  1992  Laminar Boundary Layer Flow And Heat Transfer With Favorable Pressure Gradient At Constant K Values  D. Zhou, T. Wang, Clemson University, Clemson, SC, USA;    92-GT-246 
IGTI  1992  Flow Characteristics Of A 35 Degree Inclined Turbulent Jet In A Crossflow On A Concave Surface  S.W. Lee, J.S. Lee, T.S. Lee, Seoul National University, Seoul, KOREA;    92-GT-247 
IGTI  1992  An Experimental Investigation Of Convective Heat Transfer At The Leading Edge Of A Gas Turbine Airfoil  S. Gendron, N.J. Marchand, Ecole Polytechnique, Montreal, CANADA; C. Korn, JRC Lab., Ispra, ITALY; J.P. Immarigeon, J.J. Kacprzynski, National Research Council of Canada, Ottawa, CANADA    92-GT-248 
IGTI  1992  Heat Transfer To A Rotating Drum In An Annulus With A Stator Blade Row And Axial Throughflow  P.R.N. Childs, A.B. Turner, C.M. Vaughan, D. Rayner, F.J. Bayley, University of Sussex, Brighton, GB;    92-GT-249 
IGTI  1992  MTR390 - Engine For The Future  J.S. Ducos, Turbomeca, Bordes, FRANCE; A. Spirkl, MTU Motoren & Turbinen Union GmbH, Munich, GERMANY; R. Thorn, Rolls-Royce plc, Bristol, UK    92-GT-250 
IGTI  1992  Balance Of Moments For Hypersonic Vehicles  F.G.J. Kremer, DLR - Institute of Propulsion Technology, Koln, GERMANY;    92-GT-251 
IGTI  1992  Overview Of The Japanese National Project For Super/Hyper-sonic Transport Propulsion System  O. Ichimaru, Agency of Industrial Science & Technolgy, Tokyo, JAPAN; M. Ishizuka, Matsushita Research Institute Tokyo, Inc., Tokyo, JAPAN; K. Murashima, HYPR Eng. Res. Assoc., Tokyo, JAPAN    92-GT-252 
IGTI  1992  Conceptual Design Of Turbo-Accelerator For HST Combined Cycle Engine  R. Yanagi, M. Morita, National Aerospace Laboratory, Tokyo, JAPAN; Y. Watanabe, H. Itahara, Ishikawajima-Harima Heavy Industries Co., Ltd., Tokyo, JAPAN; Y. Sasaki, Kawasaki Heavy Industries Co., Ltd., Kobe, JAPAN; T. Aoki, Mitsubishi Heavy Industries Co.    92-GT-253 
IGTI  1992  Navier-Stokes Computation On A Pivoting Doors Thrust Reverser And Comparison With Tests  L. Schreiber, SNECMA, Moissy-Cramayel, FRANCE; M. Legras, Hispano-Suiza, Harfleur, FRANCE    92-GT-254 
IGTI  1992  Ramjet NOx Emisssion - Use Of A 3D CFD Method For The Combustor Design Of A Super/Hyper-Sonic Transport Propulsion System  E. David, C. Baudoin, J.L. Schultz, D. Ansart, S. Meunier, SNECMA, Moissy-Cramayel, FRANCE;    92-GT-255 
IGTI  1992  Some Topics Of Research On Hypersonic Airbreathing Engines At National Aerospace Laboratory  K. Sakata, H. Nouse, M. Minoda, National Aerospace Laboratory, Tokyo, JAPAN;    92-GT-256 
IGTI  1992  The Influence Of Coal Slurry Fuel Properties On The Performance Of A Bench Scale Two-Stage Slagging Combustor  L.H. Cowell, C.S. Wen, R.T. LeCren, Solar Turbines Incorporated, San Diego, CA, USA;    92-GT-257 
IGTI  1992  Development Of A Direct Coal-Fired Combined Cycle For Commercial Application  R.L. Bannister, B.C. Wiant, Westinghouse Electric Corporation, Orlando, FL, USA; A.R. Jensen, F.V. Mach, E.U. Claeson, L.M. Raatikka, Northern States Power Company, Minneapolis, MN, USA; R.C. Diehl, H.M. Eppich, Textron, Inc., Everett, MA, USA; R.A. Newby    92-GT-258 
IGTI  1992  Experimental Evaluation Of A Two-Stage Slagging Combustor Design For A Coal-Fueled Industrial Gas Turbine  L.H. Cowell, R.T. LeCren, Solar Turbines Incorporated, San Diego, CA, USA;    92-GT-259 
IGTI  1992  Coal-Water Slurry Testing Of An Industrial Gas Turbine  R.A. Wenglarz, C. Wilkes, R.C. Bourke, H.C. Mongia, General Motors Corporation, Indianapolis, IN, USA;    92-GT-260 
IGTI  1992  Development Of An Indirect Coal-Fired High Performance Power Generation System  R.L. Bannister, D.J. Amos, A.J. Scalzo, Westinghouse Electric Corporation, Orlando, FL. USA; S.C. Datsko, Babcock & Wilcox, Alliance, OH, USA    92-GT-261 
IGTI  1992  Development And Industrial Application Of The "All-Over-Controlled Vortex Distribution Method" For Designing Radial And Mixed Flow Impellers  S.J. Wang, M.J. Yuan, G. Xi, S.X. Liu, D.T. Qi, X.J. Chai, Xi'an Jiaotong University, Xian, CHINA;    92-GT-262 
IGTI  1992  The Qualities Of PRENFLO Coal Gas For Use In High-Efficiency Gas Turbines  W. Schellbert, E. Kuske, Krupp Koppers GmbH, Essen, GERMANY;    92-GT-263 
IGTI  1992  Measurement Of Combustion Turbine Non-Recoverable Degradation  L.S. Flashberg, Mission Operation and Maintenance, Inc., Irvine, CA, USA; G.L. Haub, Texaco Cogeneration & Power Company, Bakersfield, CA, USA    92-GT-264 
IGTI  1992  Peaking Gas Turbine Capacity Enhancement Using Ice Storage For Compressor Inlet Air Cooling  J. Ebeling, R. Halil, Burns & McDonnell Engineering Company, Kansas City, MO, USA; D. Bantam, B. Bakenhus, Lincoln Electric System, Lincoln, NE, USA; H. Schreiber, R. Wendland, Electric Power Research Institute, Palo Alto, CA, USA    92-GT-265 
IGTI  1992  Experience With The Commissioning Of A Natural Gas Power Recovery Turbine  H.F. Stoll, RWTUV, Essen, GERMANY;    92-GT-266 
IGTI  1992  Performance Monitoring Of Gas Turbines For Failure Prevention  R.E. Dundas, Factory Mutual Engineering & Research, Norwood, MA, USA; D.A. Sullivan, Technical Innovations, Inc., Sandwich, MA, USA; F. Abegg, Golden Valley Electric Association, Inc., Fairbanks, AK    92-GT-267 
IGTI  1992  Numerical Generator Protection Offers New Benefits Of Gasturbines  M. Ilar, ABB Relays Ltd., Baden, SWITZERLAND; M. Wittwer, ABB Power Generation Ltd., Baden, SWITZERLAND    92-GT-268 
IGTI  1992  On-Line Detergent Washing: Reducing The Environmental Effects On The LCAC Gas Turbine Engines  J.S. Patterson, S.K. Spring, Naval Ship Systems Engineering Station, Philadelphia, PA, USA;    92-GT-269 
IGTI  1992  Experience With The TF40B Engine In The LCAC Fleet  E.M. House, Naval Ship Systems Engineering Station, Philadelphia, PA, USA;    92-GT-270 
IGTI  1992  1/4 Scale Hot Flow Model Test Of A GE LM2500 Exhaust System  D. Vandam, W.R. Davis Engineering Limited, Ottawa, ON, CANADA; A.M. Birk, Queen's University, Kingston, ON, CANADA    92-GT-271 
IGTI  1992  On Application Of Statistics To Verification Of Turbomachinery Calculation Methods  J. Krzyzanowski, Institute of Fluid-Flow Machinery, Gdansk, POLAND; P. Krzyslak, J. Gluch, Technical University of Gdansk, Gdansk, POLAND    92-GT-272 
IGTI  1992  Rotor Design For Large Industrial Gas Turbines  W. Endres, University of Stellenbosch, Stellenbosch, S. AFRICA;    92-GT-273 
IGTI  1992  Evaluation Of Gas Turbine Transitions After 20,000 And 37,000 Hours Of Service  V.P. Swaminathan, Southwest Research Institute, San Antonio, TX, USA; H.B. Owens, N. Hicks, ENRON Power Corporation, Houston, TX, USA    92-GT-274 
IGTI  1992  On Aerodynamic Loading Of Linear Compressor Cascades  J. Citavy, PCS Turbomachinery, Praha, CZECH;    92-GT-275 
IGTI  1992  Numerical Research On Flows In Nonuniform Cascades  F. Qi, T. Guocai, S. Chunhua, Nanjing Aeronautical Institute, Nanjing, CHINA;    92-GT-276 
IGTI  1992  Prediction Of 2D Viscous Transonic Flow In Compressor Cascades Using A Semi-Empirical Shock/Boundary-Layer Interaction Method  M. Hoeger, K.D. Broichhausen, MTU München, GERMANY;    92-GT-277 
IGTI  1992  A Simulation Of Secondary Flow In Centrifugal Impeller Channel By A Stationary Three-Dimensional Curved Duct  S. Mizuki, H. Tsujita, Hosei University, Tokyo, JAPAN;    92-GT-278 
IGTI  1992  Design Of An Incompressible High-Pressure Vaneaxial Fan Using CFD  Y.T. Lee, M.E. Slipper, David Taylor Research Center, Bethesda, MD, USA; J. Feng, C.L. Merkle, The Pennsylvania State University, University Park, PA, USA    92-GT-279 
IGTI  1992  Cold Flow Testing Of The Space Shuttle Main Engine Alternate Turbopump Development High Pressure Fuel Turbine Model  S.W. Gaddis, S.T. Hudson, NASA-Marshall Space Flight Center, Huntsville, AL, USA; P.D. Johnson, Pratt & Whitney, West Palm Beach, FL, USA    92-GT-280 
IGTI  1992  Transition Prediction In Attached And Separated Shear Layers Using An Integral Method  G. Leoutsakos, K.D. Papailiou, National Technical University, Athens, GREECE;    92-GT-281 
IGTI  1992  An Approach For Multi-Stage Calculations Incorporating Unsteadiness  M. Giles, Massachusetts Institute of Technology, Cambridge, MA, USA;    92-GT-282 
IGTI  1992  Unsteady Boundary-Layer Transition In Flow Periodically Disturbed By Wakes  U. Orth, Garrett GmbH, Raunheim, GERMANY;    92-GT-283 
IGTI  1992  Numerical And Experimental Analysis Of The Flow In A Centrifugal Pump At Nominal And Partial Flow Rate  J.F. Combes, EDF/DER, Chatou, FRANCE; E. Rieutord, INSA, Lyon, FRANCE    92-GT-284 
IGTI  1992  Potential Flow Analysis Of The Forces On A Laboratory Centrifugal Pump Impeller  S.M. Miner, United State Naval Academy, Annapolis, MD, USA; R.D. Flack, University of Virginia, Charlottesville, VA, USA; P. Trevisan, Pratt & Whitney Aircraft Group, W. Palm Beach, FL, USA    92-GT-285 
IGTI  1992  Design Of Multi-Stage Turbomachinery Blading By The Circulation Method: Actuator Duct Limit  T.Q. Dang, T. Wang, Syracuse University, Syracuse, NY, USA;    92-GT-286 
IGTI  1992  Use Of Subdomains For Inverse Problems In Branching Flow Passages  S. Krishnan, A.K. Agrawal, T.-t. Yang, Clemson University, Clemson, SC, USA;    92-GT-287 
IGTI  1992  Prediction Of Secondary Losses In Axial Compressors  V. Cyrus, SVUSS, Prague, CZECHOSLOVAKIA;    92-GT-288 
IGTI  1992  A PC-Based Inverse Design Method Applied To Radial Inflow Turbines  I.H. Skoe, Ulstein Turbine A/S, Asker, NORWAY;    92-GT-289 
IGTI  1992  A 3-D Inverse Methodology Applied To The Design Of Axisymmetric Ducts  V. Dedoussis, P. Chaviaropoulos, K.D. Papailiou, National Technical University, Athens, GREECE;    92-GT-290 
IGTI  1992  A Three-Dimensional Numerical Method For Turbomachinery Blading  C.W. Gu, J.Z. Xu, J.Y. Du, Chinese Academy of Sciences, Beijing, CHINA;    92-GT-291 
IGTI  1992  Progress On The Advanced Turbine Technology Applications Project (ATTAP), And Automotive Gas Turbine Outlook  P.J. Haley, General Motors Corporation, Indianapolis, IN, USA;    92-GT-292 
IGTI  1992  A Viscous Axisymmetric Throughflow Prediction Method For Multi-Stage Compressors  A.S. Ucer, Middle East Technical University, Ankara, TURKEY; R.P. Shreeve, Naval Postgraduate School, Monterey, CA, USA    92-GT-293 
IGTI  1992  A Simple Method For Estimating Secondary Losses In Turbines At The Preliminary Design Stage  M.B. Okan, D.G. Gregory-Smith, Durham University, Durham, ENGLAND;    92-GT-294 
IGTI  1992  Research And Development Of Ceramic Turbine Wheels  K. Watanabe, M. Masuda, T. Ozawa, M. Matsui, NGK Insulators, Ltd, Nagoya, JAPAN; K. Matsuhiro, NGK Europe GmbH, Eschborn, GERMANY    92-GT-295 
IGTI  1992  Reliability Analysis Of Structural Ceramic Components Using A Three-Parameter Weibull Distribution  S.F. Duffy, L.M. Powers, A. Starlinger, NASA LeRC, Cleveland, OH, USA;    92-GT-296 
IGTI  1992  Investigation Of Rotor Blade Roughness Effects On Turbine Performance  J.L. Boynton, R. Tabibzadeh, Rockwell International Corporation, Canogo Park, CA, USA; S.T. Hudson, NASA-Marshall Space Flight Center, Huntsville, AL, USA    92-GT-297 
IGTI  1992  A Comparison Of The Measured And Predicted Flowfield In A Modern Fan-Bypass Configuration  R.K. Goyal, General Motors Corporation, Inianapolis, IN, USA; W.N. Dawes, Cambridge University, Cambridge, UK    92-GT-298 
IGTI  1992  Investigation Of Tip Clearance Phenomena In An Axial Compressor Cascade Using Euler And Navier-Stokes Procedures  R.F. Kunz, General Motors Technical Center, Warren, MI, USA; B. Lakshminarayana, A.H. Basson, The Pennsylvania State University, University Park, PA, USA    92-GT-299 
IGTI  1992  Numerical Simulation Of Compressor Endwall And Casing Treatment Flow Phenomena  A.J. Crook, Allison Gas Turbine Division, GMC, Indianapolis, IN, USA; E.M. Greitzer, C.S. Tan, Massachusetts Institute of Technology, Cambridge, MA, USA; J.J. Adamczyk, NASA Lewis Research Center, Cleveland, OH, USA    92-GT-300 
IGTI  1992  The Role Of Laminar-Turbulent Transition In Gas Turbine Engines - A Discussion  G.J. Walker, University of Tasmania, Hobart, AUSTRALIA;    92-GT-301 
IGTI  1992  Viscous Throughflow Modelling For Multi-Stage Compressor Design  M.A. Howard, S.J. Gallimore, Rolls-Royce plc, Derby, UK;    92-GT-302 
IGTI  1992  Ingestion Into The Upstream Wheelspace Of An Axial Turbine Stage  T. Green, A.B. Turner, The University of Sussex, Sussex, UK;    92-GT-303 
IGTI  1992  Brush Seal Leakage Performance With Gaseous Working Fluids At Static And Low Rotor Speed Conditions  J.A. Carlile, R.C. Hendricks, D.A. Yoder, NASA Lewis Research Center, Cleveland, OH, USA;    92-GT-304 
IGTI  1992  The Transfer Of Heat By Self-Induced Flow In A Rotating Tube  S. Gilham, W.S. Atkins Engineering Sciences, Surrey, UK; P.C. Ivey, Cranfield Institute of Technolgy, Bedfordshire, UK; J.M. Owen, University of Bath, Bath, UK    92-GT-305 
IGTI  1992  Calculation Of Wake-Induced Unsteady Flow In A Turbine Cascade  N.-H. Cho, W. Rodi, University of Karlsruhe, Karlsruhe, GERMANY; X. Liu, Pratt & Whitney Canada, Mississauga, CANADA; B. Schonung, ABB Turbosystems, Baden, SWITZERLAND    92-GT-306 
IGTI  1992  Optimum Design Of Rotor-Bearing Systems With Eigenvalue Constraints  T.-Y. Chen, National Chung-Hsing University, Taichung, Taiwan, CHINA; B.P. Wang, The University of Texas, Arlington, TX, USA    92-GT-307 
IGTI  1992  An Investigation Of Turbulence Modelling In Transonic Fans Including A Novel Implementation Of An Implicit k-e Turbulence Model  M.G. Turner, I.K. Jennions, GE Aircraft Engines, Cincinnati, OH, USA;    92-GT-308 
IGTI  1992  Three-Dimensional Navier-Stokes Computations Of Transonic Fan Flow Using An Explicit Flow Solver And An Implicit k-e Solver  I.K. Jennions, M.G. Turner, GE Aircraft Engines, Cincinnati, OH, USA;    92-GT-309 
IGTI  1992  Infra-Red Signature Suppression For Marine Gas Turbines: Comparison Of Sea Trial And Model Test Results For The DRES Ball IRSS System  D. Vandam, W.R. Davis Engineering Limited, Ottawa, ON, CANADA; A.M. Birk, Queen's University, Kingston, ON, CANADA    92-GT-310 
IGTI  1992  Analysis Of General Electric Model 7001 First Stage Nozzle Cracking  H.L. Bernstein, R.C. McClung, T.R. Sharron, Southwest Research Institute, San Antonio, TX, USA; J.M. Allen, Electric Power Research Institute, Palo Alto, CA, USA    92-GT-311 
IGTI  1992  Powder Metallurgy Repair Of Turbine Components  K.A. Ellison, P. Lowden, J. Liburdi, Liburdi Engineering Ltd., Hamilton, ON, CANADA;    92-GT-312 
IGTI  1992  Ceramic Filters For Hot Gas Cleanup  L.R. White, T.L. Tompkins, K.C. Hsieh, D.D. Johnson, 3M Center, St. Paul, MN, USA;    92-GT-313 
IGTI  1992  Combustion System Performance And Field Test Results Of The MS7001F Gas Turbine  J.P. Claeys, K.M. Elward, W.J. Mick, R.A. Symonds, General Electric Company, Schenectady, NY, USA;    92-GT-314 
IGTI  1992  TEMPER - A Gas-Path Analysis Tool For Commercial Jet Engines  D.L. Doel, GE Aircraft Engines, Evendale, OH, USA;    92-GT-315 
IGTI  1992  Ceramic Matrix Composite Applications In Advanced Liquid Fuel Rocket Engine Turbomachinery  J.W. Brockmeyer, Rockwell International Corporation, Canoga Park, CA, USA;    92-GT-316 
IGTI  1992  Microstructural Investigations Of Plasma Sprayed YTTRIA Partially Stabilized Zirconia TBC  S. Alperine, L. Lelait, O.N.E.R.A., Chatillon, FRANCE;    92-GT-317 
IGTI  1992  Thermal Fracture Of Multilayer Ceramic Thermal Barrier Coatings  T.R. Takeuchi, K. Kokini, Purdue University, W. Lafayette, IN, USA;    92-GT-318 
IGTI  1992  Thermal Barrier Coatings On Turbine Blades By Plasma Spraying With Improved Cooling  L. Pawlowski, S. Sturlese, CSM Centro Sviluppo Materiali, Pergine di Valsugana, ITALY; T. Cosack, S. Scheiderbanger, MTU Motoren-und Turbinen-Union, München, GERMANY    92-GT-319 
IGTI  1992  Direct Measurements Of Skin Friction In Supersonic Combustion Flow Fields  K.M. Chadwick, D.J. DeTurris, J.A. Schetz, Virginia Polytechnic Institute & State University, Blacksburg, VA, USA;    92-GT-320 
IGTI  1992  Utility Perspective Of Selecting Air Filter For Simple-Cycle, Heavy-Duty Combustion Turbines  J.W. Lyons, A. Morrison, Southern Company Services, Inc., Birmingham, AL, USA;    92-GT-321 
IGTI  1992  Second-Generation Low-Emisssion Combustors For ABB Gas Turbines: Field Measurements With GT11N-EV  M. Aigner, G. Muller, ABB Power Generation Ltd., Baden, SWITZERLAND;    92-GT-322 
IGTI  1992  Measurement Of Unsteady Flow And Heat Transfer In A Linear Turbine Cascade  X. Liu, Pratt & Whitney Canada, Mississauga, CANADA; W. Rodi, University of Karlsruhe, Karlsruhe, GERMANY    92-GT-323 
IGTI  1992  Use Of Advanced CFD Codes In The Turbomachinery Design Process  O. Novak, O. Schafer, B. Schonung, ABB Turbo Systems Ltd., Baden, SWITZERLAND; H. Patzold, Interkeller Ltd., Bruttisellen, SWITZERLAND    92-GT-324 
IGTI  1992  Meridional Flow Calculation Using Advanced CFD Techniques  P. Kiousis, P. Chaviaropoulos, K.D. Papiliou, National Technical University of Athens, Athens, GREECE;    92-GT-325 
IGTI  1992  Effect Of Manufacturing Deviations On Performance Of Axial Flow Compressor Blading  E. Marson, Westinghouse Canada Inc., Hamilton, CANADA;    92-GT-326 
IGTI  1992  A Summary Of Allison Gas Turbine's Marine Experience  J.S. Weisert, General Motors Corporation, Indianapolis, IN, USA;    92-GT-327 
IGTI  1992  The Redesign Of A Marine Gas Turbine Generator Set  P. Cheney, National Defence Headquarters, Ottawa, CANADA; A. Abdelrazik, Naval Engineering Test Establishment, Montreal, CANADA    92-GT-328 
IGTI  1992  The U.S. Navy's Design, Development And Implementation Program For Gas Turbine Generator Sets  J.J. McGroarty, Naval Ship Systems Engineering Station, Philadelphia, PA, USA;    92-GT-329 
IGTI  1992  A Conceptual Design For A Combined Cycle Power Plant Comprising Modified Exhaust-Heated Gas Turbine And A Steam Turbine Plant - Part I: Preliminary Calculations, Basic Dimensions, And General Design Conception  J.A. Golinski, Technical University, Wroclaw, POLAND;    92-GT-330 
IGTI  1992  A New Approach To The Design Of Combined Cycle Plants  T. Wiekmeijer, Prometheus Energy Systems B.V., THE NETHERLANDS;    92-GT-331 
IGTI  1992  Evolution And Introduction Of The MARS T-14000 Gas Turbine  C.M. Waldhelm, Solar Turbines Incorporated, San Diego, CA, USA;    92-GT-332 
IGTI  1992  Assessing The Economics Of Industrial Gas Turbine Cogeneration Applications  J.P. Hill, Georgia Power Company, Atlanta, GA, USA;    92-GT-333 
IGTI  1992  Durability Surveillance Program On The Advanced Gas Turbine GE Frame 7 F  I.S. Ondryas, Fluor Daniel Power, Irvine, CA, USA; C. Meher-Homji, Boyce Engineering International, Houston, TX, USA; P. Boehler, Potomac Electric Power company, Dickerson, MD, USA; C. Dohner, Electric Power Research Institute, Palo Alto, CA, USA;    92-GT-334 
IGTI  1992  MS5002 Advanced Technology Uprate And Field Modification Experience  Ismoyo, P.T. Arun NGL Co., Lhokeseumawe, INDONESIA; C.M. Grondahl, General Electric Company, Schenectady, NY, USA; C.D. Kinney, Mobil Exploration & Producing Services, Inc., Dallas, TX, USA    92-GT-335 
IGTI  1992  The VKI Compression Tube Annular Cascade Facility CT3  C.H. Sieverding, T. Arts, Von Karman Institute for Fluid Dynamics, Rhode-St-Genese, BELGIUM;    92-GT-336 
IGTI  1992  An Opto-Electronic Data Transmission System For Measurements On Rotating Turbomachinery Components  C.H. Sieverding, C. Vanhaeverbeek, G. Schulze, Von Karman Institute for Fluid Dynamics, Rhode-St-Genese, BELGIUM;    92-GT-337 
IGTI  1992  High Nitrogen Martensitic Steels - A New Family Of Martensitic Corrosion Resistant Steels For Improved Aerospace Bearing Performance  W. Trojahn, FAG Kugelfischer KGaA, Schweinfurt, GERMANY;    92-GT-338 
IGTI  1992  Some Basic Reflections About The Influence Of Non-Metallic Inclusions On Rolling Contact Fatigue Of Bearing Steels  H.-J. Bohmer, FAG Kugelfischer KGaA, Schweinfurt, GERMANY;    92-GT-339 
IGTI  1992  Advanced Blading For Last Stages Of Heavy Duty Gas Turbines - A Joint German Action  U. Pickert, K.H. Keienburg, Siemens/KWU, Mulheim, GERMANY; R. Burgel, K. Schneider, ABB Kraftwerke, Mannheim, GERMANY    92-GT-340 
IGTI  1992  Mechanical Properties, Oxidation Resistance And Their Interaction For Two Gas Turbine Seal Ring Alloys  S.K. Srivastava, Haynes Internaitonal, Inc., Kokomo, IN, USA;    92-GT-341 
IGTI  1992  Thermomechnaical Damage Development In SiC(SCS6)/Ti-64 Metal Matrix Composite  S. Aksoy, Textron Lycoming, Stratford, CT, USA;    92-GT-342 
IGTI  1992  Study Of Pressurized Fluidized Bed Combustion Combined Cycles With Gas Turbine Topping Cycle  D. Bohn, G.H. Dibelius, R.U. Pitt, R. Faatz, Institut fur Dampf-und Gasturbinen, Aachen, GERMANY; G. Cerri, C. Salvini, Universita degli studi di Roma, Rome, ITALY    92-GT-343 
IGTI  1992  An Automotive Gas Turbine Engine Blade Erosion  M. Metwally, W. Tabakoff, A. Hamed, University of Cincinnati, Cincinnati, OH, USA;    92-GT-344 
IGTI  1992  Turbine Cascade Optimization Against Particle Deposition  D.D. Kladas, D.P. Georgiou, University of Patras, Patras, GREECE;    92-GT-345 
IGTI  1992  Concentration Fluctuations In Turbulent Cross Jet Mixing  G.E. Andrews, U.S. Abdul Hussain, University of Leeds, Leeds, UK;    92-GT-346 
IGTI  1992  The Comparison Of Different Simplified Mathematical Models Of The Gas Turbine Combustion Chamber As An Object Of Temperature And Pressure Control  M. Dzida, Technical University of Gdansk, Gdansk, POLAND;    92-GT-347 
IGTI  1992  Fiber-Reinforced Composites For Gas Turbine Applications  D.P. Stinton, R.A. Lowden, T.M. Besmann, Oak Ridge National Laboratory, Oak Ridge, TN, USA;    92-GT-348 
IGTI  1992  Experimental Study Of Mixed Compression Air-Intake For Hypersonic Airbreathing Engines  K. Sakata, R. Yanagi, A. Murakami, S. Shindo, National Aerospace Laboratory, Tokyo, JAPAN; S. Honami, Science University of Tokyo, Tokyo, JAPAN; A. Tanaka, D. Shiraishi, Ishikawajima-Harima Heavy Industry, Tokyo, JAPAN    92-GT-349 
IGTI  1992  Magnetic Particle Inspection Of Turbine Blades In Power Generating Plants  C. Imbert, University of the West Indies, St. Augustine, TRINIDAD; K. Rampersad, Trinidad & Tobago Electricity Commission, Port-of-Spain, TRINIDAD    92-GT-350 
IGTI  1992  Optimization Of An Advanced Combined Cycle And Its Application To The Yokohama Thermal Power Station No. 7 And No. 8 Groups  Z. Aizawa, Tokyo Electric Power Company, Tokyo, JAPAN; W. Carberg, General Electric Company, Schenectady, NY, USA    92-GT-351 
IGTI  1992  Past And Future Of Industrial Cogeneration In The Netherlands  K. Blok, W.C. Turkenburg, University of Utrecht, Utrecht, NETHERLANDS;    92-GT-352 
IGTI  1992  Technical And Economical Aspects Of Using Gas Turbine Technology In Eastern Europe Including The Commonwealth Of Independent States (CIS)  B. Boehm, R.-R. Marks, Siemens Power Generation Group, Erlangen, GERMANY;    92-GT-353 
IGTI  1992  Trial Operations Of Unit No. 1 Group 690 MW Combined Cycle Power Plant Of Shin-Oita Power Station  S. Nogami, Kyushu Electric Power Co., Inc., Oita, JAPAN; N. Ando, Hitachi Ltd., Tokyo, JAPAN; Y. Noguchi, K. Takahashi, T. Iwamiya, Y. Hattori, Hitachi Ltd., Hitachi, JAPAN    92-GT-354 
IGTI  1992  A Combined Experimental And Theoretical Study Of Flow And Pressure Distributions In A Brush Seal  F.J. Bayley, C.A. Long, The University of Sussex, Sussex, UK;    92-GT-355 
IGTI  1992  Separated Flow In A Low Speed Two-Dimensional Cascade: Part I - Flow Visualization And Time-Mean Velocity Measurements  A.M. Yocum, Pennsylvania State University, State College, PA, USA; W.F. O'Brien, VA Polytechnic Institute & State University, Blacksburg, VA, USA    92-GT-356 
IGTI  1992  Separated Flow In A Low Speed Two-Dimensional Cascade: Part II - Cascade Performance  A.M. Yocum, Pennsylvania State University, State College, PA, USA; W.F. O'Brien, VA Polytechnic Institute & State University, Blacksburg, VA, USA    92-GT-357 
IGTI  1992  A Study Of Rotor Cavities And Heat Transfer In A Cooling Process In A Gas Turbine  R.S. Amano, V. Pavelic, University of Wisconsin, Milwaukee, WI, USA;    92-GT-358 
IGTI  1992  Coal Gas Cleaning And Purification With Inorganic Membranes  D.E. Fain, G.E. Roettger, Martin Marietta Energy Systems, Inc., Oak Ridge, TN, USA;    92-GT-359 
IGTI  1992  Performance Of Gasturbine Compressor Cleaners  H.J. Kolkman, National Aerospace Laboratory NLR, Amsterdam, NETHERLANDS;    92-GT-360 
IGTI  1992  Models For Predicting The Performance Of Brayton-Cycle Engines  T. Korakianitis, Washington University, St. Louis, MO, USA; D.G. Wilson, M.I.T., Cambridge, MA, USA    92-GT-361 
IGTI  1992  Thrust Vectoring/Reversing Tactics In Air-To-Air Combat  C.W. Boppe, R.P. Martorella, Grumman Corporation, Bethpage, NY, USA;    92-GT-362 
IGTI  1992  The Extension Of A Solution-Adaptive 3D Navier-Stokes Solver Towards Geometries Of Arbitrary Complexity  W.N. Dawes, Whittle Laboratory, Cambridge, U.K.;    92-GT-363 
IGTI  1992  Radial Transport And Momentum Exchange In An Axial Compressor  R.P. Dring, United Technologies Research Center, E. Hartford, CT, USA;    92-GT-364 
IGTI  1992  A High Speed Capacitance Based System For Gauging Turbomachinery Blading Radius During The Tip Grind Process  A.G. Sheard, G.C. Westerman, B. Killeen, Rotodata Limited, Derby, ENGLAND; M. Fitzpatrick, Dean, Smith, & Grace Ltd, West Yorkshire, ENGLAND    92-GT-365 
IGTI  1992  Prescribed-Curvature-Distribution Airfoils For The Preliminary Geometric Design Of Axial-Turbomachinery Cascades  T. Korakianitis, Washington University, St. Louis, MO, USA;    92-GT-366 
IGTI  1992  An Automated Flow Line For Gas Turbine Blade Repair  D.B. Doll, United Airlines Maintenance Operations Division, San Francisco, CA, USA;    92-GT-367 
IGTI  1992  HVOF Spraying And Laser Processing Of Waspaloy Thick Films  A. Adamski, Northwest University, Evanston, IL, USA; R. Bamola, TMT, Houston, TX, USA; L. Hultman, Linkoping University, Linkoping, SWEDEN    92-GT-368 
IGTI  1992  Erosion Characteristics Of Ceramic Particulate And Whisker Reinforced Aluminum Composites  S. Gupta, Rolls-Royce Inc., Atlanta, GA, USA;    92-GT-369 
IGTI  1992  Development Of High Temperature High Pressure Filtration Technology  K. Higashi, N. Oda, Asahi Glass Company, Ltd., JAPAN;    92-GT-370 
IGTI  1992  The Flame Structure Of High INtensity Multi-Jet Shear Layer Enclosed Turbulent Diffusion Flames  G.E. Andrews, A.F. Ali Al-Shaikhly, The University of Leeds, Leeds, UK;    92-GT-371 
IGTI  1992  Direct Numerical Simulation Of Nitric Oxyde Evolution In Underexpanded Jets  R.J. Gathmann, C. Baudoin, J.P. Chollet, Inst. de Mecanique de Grenoble, Grenoble, FRANCE;    92-GT-372 
IGTI  1992  Massive Steam Injection On An MS6001B Gas Turbine In Cogeneration Service  K.M. Elward, D.A. Flodman, R.A. Symonds, General Electric Company, Schenectady, NY, USA;    92-GT-373 
IGTI  1992  On The Concept Of Durability In Evaluation Of Equipment Life-Cycle Cost  I.S. Ondryas, Fluor Daniel Power, Irvine, CA, USA;    92-GT-374 
IGTI  1992  Mechanical Design Of Free Standing Exhaust Stacks For Offshore Applications  I.M. Allison, University of Surrey, Guildford, ENGLAND; A.C. Steel, Altair Filters International Ltd., Hampshire, ENGLAND    92-GT-375 
IGTI  1992  Combined Cycle Power Plant Start-Up Effects And Constraints Of The HRSG  A. Pasha, Henry Vogt Machine Company, Louisville, KY, USA;    92-GT-376 
IGTI  1992  The Effects Of Incident Turbulence And Moving Wakes On Laminar Heat Transfer In Gas Turbines  K. Dullenkopf, University of Karlsruhe, Karlsruhe, GERMANY; R.E. Mayle, Rensselaer Polytechnic Institute, Troy, NY, USA    92-GT-377 
IGTI  1992  Rotor Cavity Flow And Heat Transfer With Inlet Swirl And Radial Outflow Of Cooling Air  F.W. Staub, GE Corporate Research & Development, Schenectady, NY, USA;    92-GT-378 
IGTI  1992  Effective Sealing Of A Disk Cavity Using A Double-Toothed Rim Seal  S.H. Bhavnani, V.I. Khilnani, L.-C. Tsai, J.M. Khodadadi, J.S. Goodling, Auburn University, Auburn, AL, USA; J. Waggott, Dresser-Rand, Wellsville, NY, USA    92-GT-379 
IGTI  1992  Effects Of Free-Stream Turbulence And Adverse Pressure Gradients On Boundary Layer Transition  J.P. Gostelow, A.R. Blunden, University of Technology, Sydney, AUSTRALIA; G.J. Walker, University of Tasmania, Hobart, AUSTRALIA    92-GT-380 
IGTI  1992  ATTAP Ceramic Gas Turbine Technology Development  J.R. Smyth, R.E. Morey, Allied-Signal Aerospace Company, Phoenix, AZ, USA;    92-GT-381 
IGTI  1992  An Externally Pressurized Air Bearing System, Journals And Thrust, For Application To Small Turbomachinery  A.B. Turner, S.J. Davies, Y.L. Nimir, J.D. Richardson, University of Sussex, Sussex, UK;    92-GT-382 
IGTI  1992  Ceramic Component Reliability With The Restructured NASA/CARES Computer Program  L.M. Powers, A. Starlinger, J.P. Gyekenyesi, NASA-LeRC, Cleveland, OH, USA;    92-GT-383 
IGTI  1992  Evaluation Of Fast Fracture Strength Of Ceramic Components Under Multiaxial Stress States  H. Uchimura, A. Kokaji, M. Kaji, Kyocera Corporation, Kagoshima, JAPAN;    92-GT-384 
IGTI  1992  Selection, Development, And Application Of Forming And Densification Techniques For Silicon Nitride Heat Engine Components  J. Pollinger, B. Busovne, M. Meiser, J. Nick, Allied-Signal Aerospace Company, Torrance, CA, USA;    92-GT-385 
IGTI  1992  Development And Application Of A Low Cost Integrated Based System For The Operation And Condition Based Maintenance Of Gas Turbines  H.C. Higgins, J.L. Hackett, British Gas plc., Leicestershire, ENGLAND;    92-GT-386 
IGTI  1992  Development And Operation Of Remotely Controlled Modular Gas Turbine Driven Compressor Stations  C.J. Austin, H.C. Higgins, British Gas plc., Leicestershire, ENGLAND;    92-GT-387 
IGTI  1992  Analysis Of Three-Dimensional Viscous Flow In A Supersonic Axial Flow Compressor Rotor With Emphasis On Tip Leakage Flow  G. Perrin, F. Leboeuf, Ecole Centrale de Lyon, Ecully, FRANCE; W.N. Dawes, Cambridge University, Cambridge, ENGLAND    92-GT-388 
IGTI  1992  Second-Order Effects Of Unsteadiness On The Performance Of Turbomachines  G. Fritsch, M. Giles, Massachusetts Institute of Technology, Cambridge, MA, USA;    92-GT-389 
IGTI  1992  Flow Studies In Ducted Twin-Rotor Contra-Rotating Axial Flow Fans  B. Roy, D. Ravibabu, P. Srinivasa Rao, S. Basu, A. Raju, P.N. Murthy, IIT, Bombay, INDIA;    92-GT-390 
IGTI  1992  LV100 AIPS Technology - For Future Army Propulsion  W. Brockett, Textron Lycoming, Stratford, CT, USA; A. Koschier, General Electric, Lynn, MA, USA    92-GT-391 
IGTI  1992  Improving Dynamic Response Of A Single-Spool Gas Turbine Engine Using A Nonlinear Controller  O.F. Qi, N.R.L. Maccallum, P.J. Gawthrop, University of Glasgow, Glasgow, UK;    92-GT-392 
IGTI  1992  Impact Of Ceramic Components In Gas Turbines For Industrial Cogeneration  D. Anson, W. Sheppard, Battelle Memorial Institute, Columbus, OH, USA; W. Parks, Jr., U.S. Department of Energy, Washington, D.C., USA    92-GT-393 
IGTI  1992