GT-2002-30275 Gas Turbine Performance Prediction by Using Generalized Performance Curves of Compressor and Turbine Stages (English)
- New search for: Spina, P. R.
- New search for: ASME
- New search for: Spina, P. R.
- New search for: ASME
In:
ASME turbo expo 2002
;
1073-1082
;
2002
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ISBN:
- Conference paper / Print
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Title:GT-2002-30275 Gas Turbine Performance Prediction by Using Generalized Performance Curves of Compressor and Turbine Stages
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Contributors:Spina, P. R. ( author ) / ASME
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Conference:ASME turbo expo 2002 ; 2002 ; Amsterdam, The Netherlands
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Published in:ASME turbo expo 2002 ; 1073-1082PROCEEDINGS OF THE ASME TURBO EXPO ; 2b ; 1073-1082
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Publisher:
- New search for: ASME
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Publication date:2002-01-01
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Size:10 pages
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Remarks:Theme title: Gas turbines for a better tomorrow
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ISBN:
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Type of media:Conference paper
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Type of material:Print
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Language:English
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Keywords:
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Source:
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Table of contents conference proceedings
The tables of contents are generated automatically and are based on the data records of the individual contributions available in the index of the TIB portal. The display of the Tables of Contents may therefore be incomplete.
- 1
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GT-2002-30019 Feed Forward Neural Network-Based Diagnostic Tool for Gas Turbine Power PlantDambrosio, L. / Bomba, M. / Camporeale, S. M. / Fortunato, B. / ASME et al. | 2002
- 1
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Feed forward neural network-based diagnostic tool for gas turbine power plantDambrosio, L. / Bomba, M. / Camporeale, S.M. / Fortunato, B. et al. | 2002
- 9
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GT-2002-30020 Identifiability in Multi-Point Gas Turbine Parameter Estimation ProblemsGronstedt, T. U. J. / ASME et al. | 2002
- 19
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GT-2002-30021 Fault Diagnostics Using Genetic Algorithm for Advanced Cycle Gas TurbineSampath, S. / Gulati, A. / Singh, R. / ASME et al. | 2002
- 19
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Fault diagnostics using genetic algorithm for advanced cycle gas turbineSampath, S. / Gulati, A. / Singh, R. et al. | 2002
- 29
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GT-2002-30022 Application of an Advanced Performance Monitoring System to Detect an Implanted Fault on a Twin Spool Aero Derived Gas TurbineRazak, A. M. Y. / Dosanjh, M. S. / ASME et al. | 2002
- 37
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GT-2002-30023 Performance Monitoring on the Asgard "A" FPSO as Part of an Integrated Monitoring StrategySorli, A. / Langnes, K. / Laagland, G. / Hastings, M. / ASME et al. | 2002
- 45
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GT-2002-30024 Gas Turbine Data Validation Using Gas Path AnalysisEscher, P. C. / ASME et al. | 2002
- 45
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Gas turbine data validation using gas path analysisEscher, P.C. et al. | 2002
- 53
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GT-2002-30025 Interpretation of a Weighted-Least-Squares Gas Path Analysis ResultsDoel, D. L. / ASME et al. | 2002
- 53
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Interpretation of weighted-least-squares gas path analysis resultsDoel, D.L. et al. | 2002
- 65
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GT-2002-30026 Turbofan Performance Deterioration Tracking Using Non-Linear Models and Optimization TechniquesMathioudakis, K. / Kamboukos, P. / Stamatis, A. / ASME et al. | 2002
- 75
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GT-2002-30027 A Review of Gas Turbine Flow Path Analysis: From Paper Calculation to Artificial Neural NetworksGenrup, M. / Assadi, M. / Torisson, T. / ASME et al. | 2002
- 83
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GT-2002-30028 Application of a Preprocessed Classifier Type Neural Network for Searching of Faulty Components of Power Cycles in Case of Incomplete Measurement DataGluch, J. / Krzyzanowski, J. / ASME et al. | 2002
- 93
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Automated fault diagnosis for small gas turbine enginesDavison, C.R. / Birk, A.M. et al. | 2002
- 93
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GT-2002-30029 Automated Fault Diagnosis for Small Gas Turbine EnginesDavison, C. R. / Birk, A. M. / ASME et al. | 2002
- 101
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GT-2002-30030 Setting Up of a Probabilistic Neural Network for Sensor Fault Detection Including Operation With Component FaultsRomessis, C. / Mathioudakis, K. / ASME et al. | 2002
- 109
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GT-2002-30031 Non-Linear Engine Component Fault Diagnosis From a Limited Number of Measurements Using a Combinatorial ApproachAretakis, N. / Mathioudakis, K. / Stamatis, A. / ASME et al. | 2002
- 119
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GT-2002-30032 Increasing Diagnostic Effectiveness by Inclusion of Fuel Composition and Water Injection EffectsMathioudakis, K. / Aretakis, N. / Tsalavoutas, A. / ASME et al. | 2002
- 127
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GT-2002-30033 The Use of Expert Systems for Gas Turbine Diagnostics and MaintenanceSpina, P. R. / Torella, G. / Venturini, M. / ASME et al. | 2002
- 135
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GT-2002-30034 Upgrading Engine Test Cells for Improved Troubleshooting and DiagnosticsRoemer, M. J. / Orsagh, R. F. / Kacprzynski, G. J. / Scheid, J. / Friend, R. / Sotomayer, W. / ASME et al. | 2002
- 145
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GT-2002-30035 Nonlinear Gas Turbine Modeling Using Feedforward Neural NetworksChiras, N. / Evans, C. / Rees, D. / ASME et al. | 2002
- 153
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GT-2002-30036 Application of Dynamic Simulation to CAES G/T Control System DevelopmentTakahashi, K. / Yasuda, T. / Endoh, M. / Kurosaki, M. / ASME et al. | 2002
- 163
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GT-2002-30038 Application of Markov Chains to Identification of Turbine Engine Dynamic ModelsArkov, V. Y. / Kulikov, G. G. / Breikin, T. V. / ASME et al. | 2002
- 169
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A high-fidelity real-time simulation code of gas turbine dynamics for control applicationsCamporeale, S.M. / Fortunato, B. / Mastrovito, M. et al. | 2002
- 169
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GT-2002-30039 A High-Fidelity Real-Time Simulation Code of Gas Turbine Dynamics for Control ApplicationsCamporeale, S. M. / Fortunato, B. / Mastrovito, M. / ASME et al. | 2002
- 183
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GT-2002-30040 Staged Combustion Control System Development for Aviation Gas Turbine EnginesBreikin, T. V. / Hargrave, S. M. / Thompson, H. A. / Fleming, P. J. / Riley, S. J. / ASME et al. | 2002
- 189
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GT-2002-30041 A Model-Based Controller for Commercial Aero Gas TurbinesTurevskiy, A. / Meisner, R. / Luppold, R. H. / Kern, R. A. / Fuller, J. W. / ASME et al. | 2002
- 197
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Active combustion instability control with spinning valve actuatorBarooah, P. / Anderson, T.J. / Cohen, J.M. et al. | 2002
- 197
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GT-2002-30042 Active Combustion Instability Control With Spinning Valve ActuatorBarroah, P. / Anderson, T. J. / Cohen, J. M. / ASME et al. | 2002
- 209
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GT-2002-30043 Thermocouple Probes for Accurate Temperature Measurements in Short Duration FacilitiesPaniagua, G. / Denos, R. / Oropesa, M. / ASME et al. | 2002
- 209
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Thermocouple probes for accurate temperature measurements in short duration facilitiesPaniagua, G. / Denos, R. / Oropesa, M. et al. | 2002
- 219
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GT-2002-30044 An Optimized Pneumatic Probe for Investigation of Gas Turbine Aerodynamics in Full Scale Gas TurbinesWarnack, D. / ASME et al. | 2002
- 219
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An optimized pneumatic probe for investigation of gas turbine aerodynamics in full scale gas turbinesWarnack, D. et al. | 2002
- 227
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GT-2002-30045 Considerations for Using 3D Pneumatic Probes in High Speed Axial CompressorsColdrick, S. / Ivey, P. / Wells, R. / ASME et al. | 2002
- 235
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An air-cooled jacket designed to protect unsteady pressure transducers at elevated temperatures in gas turbine enginesIvey, P.C. / Ferguson, D.G. et al. | 2002
- 235
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GT-2002-30046 An Air-Cooled Jacket Designed to Protect Unsteady Pressure Transducers at Elevated Temperatures in Gas Turbine EnginesIvey, P. C. / Ferguson, D. G. / ASME et al. | 2002
- 243
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GT-2002-30047 Gas Turbine Corrected Parameters Control - Humidity Correction - Sensors Evaluation and SelectionArar, M. I. / ASME et al. | 2002
- 243
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Gas turbine corrected parameter control - Humidity correction - Sensors evaluation and selectionArar, M.I. et al. | 2002
- 255
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Modern telemetry systems and rotating instrumentationZeisberger, A. / Matziol, L. / Deubert, F. et al. | 2002
- 255
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GT-2002-30048 Modern Telemetry Systems and Rotating InstrumentationZeisberger, A. / Matziol, L. / Deubert, F. / ASME et al. | 2002
- 261
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GT-2002-30049 Computational Comparison of the RB199 and GE90 Pyrometer Purging SystemsKerr, C. / Ivey, P. / Oxley, N. / ASME et al. | 2002
- 271
-
Study of the optimisation of measurement sets for gas path fault diagnosis in gas turbinesOgaji, S.O.T. / Singh, R. et al. | 2002
- 271
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GT-2002-30050 Study of the Optimisation of Measurement Sets for Gas Path Fault Diagnosis in Gas TurbinesOgaji, S. O. T. / Singh, R. / ASME et al. | 2002
- 281
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GT-2002-30051 Innovative Minimally Intrusive Sensor Technology Development for Versatile Affordable Advanced Turbine Engine CombustorsGoldstein, N. / Arana, C. A. / Bien, F. / Lee, J. / Gruninger, J. / Anderson, T. / Glasheen, W. M. / ASME et al. | 2002
- 281
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Innovative minimally intrusive sensor technology development for versatile affordable advanced turbine engine combustorsGoldstein, N. / Arana, C.A. / Bien, F. / Lee, J. / Gruninger, J. / Anderson, T. / Glasheen, W.M. et al. | 2002
- 289
-
Observations of flame behavior in a laboratory-scale pre-mixed natural gas/air gas turbine combustor from PLIF measurements of OHHedman, P.O. / Fletcher, T.H. / Graham, S.G. / Timothy, G.W. / Flores, D.V. / Haslam, J.K. et al. | 2002
- 289
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GT-2002-30052 Observations of Flame Behavior in a Laboratory-Scale Pre-Mixed Natural Gas/Air Gas Turbine Combustor From PLIF Measurements of OHHedman, P. O. / Fletcher, T. H. / Graham, S. G. / Timothy, G. W. / Flores, D. V. / Haslam, J. K. / ASME et al. | 2002
- 301
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Observations of flame behavior in a laboratory-scale pre-mixed natural gas/air gas turbine combustor from LDA velocity measurementsHedman, P.O. / Murray, R.L. / Fletcher, T.H. et al. | 2002
- 301
-
GT-2002-30053 Observations of Flame Behavior in a Laboratory-Scale Pre-Mixed Natural Gas/Air Gas Turbine Combustor From LDA Velocity MeasurementsHedman, P. O. / Murray, R. L. / Fletcher, T. H. / ASME et al. | 2002
- 313
-
Observations of flame behavior in a laboratory-scale pre-mixed natural gas/air gas turbine combustor from cars temperature measurementsHedman, P.O. / Flores, D.V. / Fletcher, T.H. et al. | 2002
- 313
-
GT-2002-30054 Observations of Flame Behavior in a Laboratory-Scale Pre-Mixed Natural Gas/Air Gas Turbine Combustor From CARS Temperature MeasurementsHedman, P. O. / Flores, D. V. / Fletcher, T. H. / ASME et al. | 2002
- 323
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GT-2002-30055 TINTELL: An Innovative Method for Blade Life ManagementHunik, R. / Rooth, R. A. / ASME et al. | 2002
- 333
-
GT-2002-30109 Performance Evaluation of Multi-Stage SOFC and Gas Turbine Combined SystemsNishida, K. / Takagi, T. / Kinoshita, S. / Tsuji, T. / ASME et al. | 2002
- 341
-
GT-2002-30110 Dynamic Modeling Results of a 1MW Molten Carbonate Fuel Cell/Gas Turbine Power SystemLiese, E. / Gemmen, R. S. / ASME et al. | 2002
- 351
-
GT-2002-30111 Performance Evaluation of Gas Turbine-Fuel Cell Hybrid Micro Generation SystemKimijima, S. / Kasagi, N. / ASME et al. | 2002
- 361
-
Assessment of the potential of combined micro gas turbine and high temperature fuel cell systemsBohn, D. / Poppe, N. / Lepers, J. et al. | 2002
- 361
-
GT-2002-30112 Assessment of the Potential of Combined Micro Gas Turbine and High Temperature Fuel Cell SystemsBohn, D. / Poppe, N. / Lepers, J. / ASME et al. | 2002
- 371
-
GT-2002-30113 Molten Carbonate Fuel Cell Gas Turbine Combined Cycle for Marine Propulsion: Part B - Part Load OperationBasurto, M.-T. / Pilidis, P. / Hales, R. / ASME et al. | 2002
- 379
-
GT-2002-30114 Molten Carbonate Fuel Cell Gas Turbine Combined Cycle for Marine Propulsion: Part A - Design Point OperationBasurto, M.-T. / Pilidis, P. / Hales, R. / ASME et al. | 2002
- 387
-
GT-2002-30115 Off-Design Performance Analysis of a Hybrid System Based on an Existing MCFC StackBedont, P. / Grillo, O. / Massardo, A. F. / ASME et al. | 2002
- 397
-
GT-2002-30116 The R-ATR and the R-REF Gas Turbine Power Cycles With CO~2 Removal: Part 1 - The R-ATR CycleFiaschi, D. / Lombardi, L. / Tapinassi, L. / ASME et al. | 2002
- 405
-
GT-2002-30117 Thermodynamic Performance Analysis of New Gas Turbine Combined Cycles With No Emissions of Carbon DioxideGabbrielli, R. / Singh, R. / ASME et al. | 2002
- 405
-
Thermodynamic performance analysis of new gas turbine combined cycles with no emissions of carbon dioxideGabbrielli, R. / Singh, R. et al. | 2002
- 413
-
Conceptual design for an industrial prototype GRAZ CYCLE power plantJericha, H. / Gottlich, E. et al. | 2002
- 413
-
GT-2002-30118 Conceptual Design for an Industrial Prototype Graz Cycle Power PlantJericha, H. / Gottlich, E. / ASME et al. | 2002
- 421
-
GT-2002-30119 The Chronological Development of the Cheng Cycle Steam Injected Gas Turbine During the Past 25 YearsCheng, D. Y. / Nelson, A. L. C. / ASME et al. | 2002
- 429
-
GT-2002-30120 Thermoeconomic Analysis of a Gas Turbine Plant With Fuel Decarbonization and Dioxide SequestrationBozzolo, M. / Brandani, M. / Traverso, A. / Massardo, A. F. / ASME et al. | 2002
- 439
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GT-2002-30123 A Fifty Percent Plus Efficiency Mid Range Advanced Cheng CycleNelson, A. L. C. / Vaezi, V. / Cheng, D. Y. / ASME et al. | 2002
- 447
-
GT-2002-30124 Cost Optimization of Water Recovery Systems for Steam Injected Gas TurbinesBlanco, G. / Ambs, L. L. / ASME et al. | 2002
- 457
-
GT-2002-30125 Exergy Analysis of Part Flow Evaporative Gas Turbine Cycles: Part 1 - Introduction and MethodJonsson, M. / Yan, J. / ASME et al. | 2002
- 465
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GT-2002-30126 Exergy Analysis of Part Flow Evaporative Gas Turbine Cycles: Part 2 - Results and DiscussionJonsson, M. / Yan, J. / ASME et al. | 2002
- 475
-
GT-2002-30127 Experimental and Theoretical Results of a Humidification Tower in an Evaporative Gas Turbine Cycle Pilot PlantLindquist, T. / Thern, M. / Torisson, T. / ASME et al. | 2002
- 485
-
GT-2002-30128 Novel EFHAT System With Enhancement of Humidification by Recovery of GT Exhaust Latent HeatJin, H. / Zhao, H. / Liu, Z. / Deng, S. / Cai, R. / ASME et al. | 2002
- 493
-
GT-2002-30129 Inherent CO~2 Capture Using Chemical Looping Combustion in a Natural Gas Fired Power CycleBrandvoll, O. / Bolland, O. / ASME et al. | 2002
- 501
-
GT-2002-30131 Optimisation of Biomass Fuelled Gas Turbines Using Genetic AlgorithmsFerreira, S. B. / Pilidis, P. / Widell, H. / ASME et al. | 2002
- 501
-
Optimisation of biomass fuelled gas turbines using genetic algorithmsFerreira, S.B. / Pilidis, P. / Widell, H. et al. | 2002
- 509
-
GT-2002-30132 Comparative Analysis of Off-Design Performance Characteristics of Single and Two Shaft Industrial Gas TurbinesKim, J. H. / Kim, T. S. / Sohn, J. L. / Ro, S. T. / ASME et al. | 2002
- 517
-
GT-2002-30133 Improved Gas Turbine Efficiency Through Alternative Regenerator ConfigurationDelleback, P. A. / ASME et al. | 2002
- 517
-
Improved gas turbine efficiency through alternative regenerator configurationDellenback, P.A. et al. | 2002
- 527
-
GT-2002-30135 Steady and Dynamic Performance and Emissions of a Variable Geometry Combustor in a Gas Turbine EngineLi, Y. G. / Hales, R. L. / ASME et al. | 2002
- 537
-
GT-2002-30136 Part Load Behavior Optimization of Hybrid Coal and Gas Fired Combined Cycles Including Deactivation of ComponentsKuhnel, J. / Abhari, R. S. / ASME et al. | 2002
- 547
-
GT-2002-30137 An Alternative Cruising Method (Constant Speed) for the Hercules C-130H: Relative Life Savings When Compared to the Constant Power One and the Effect of Several Engine Physical FaultsKotsipoulos, P. / Singh, R. / Templalexis, I. / ASME et al. | 2002
- 557
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Noise reduction from engine tests at airportsAdkins, R. et al. | 2002
- 557
-
GT-2002-30138 Noise Reduction From Engine Tests at AirportsAdkins, R. / ASME et al. | 2002
- 563
-
A new generalised carbon exergy tax: An effective rule to control global warmingTraverso, A. / Massardo, A.F. / Santarelli, M. / Cali, M. et al. | 2002
- 563
-
GT-2002-30139 A New Generalised Carbon Exergy Tax: An Effective Rule to Control Global WarmingTraverso, A. / Massardo, A. F. / Santarelli, M. / Cali, M. / ASME et al. | 2002
- 571
-
GT-2002-30140 Brayton or Bayton-Rankine Combined Cycle With Hot-Gas Recirculation and Inverse Mixing EjectorStankovic, B. / ASME et al. | 2002
- 581
-
GT-2002-30141 Complex Energy Systems Exploiting Solar Energy and Natural Gas VaporizationBisio, G. / Bosio, A. / Cartesegna, M. / Rubatto, G. / ASME et al. | 2002
- 591
-
GT-2002-30144 Equipment of a Sister Ship of Aircraft Carrier Charles De Gaulle With 2 HTR Nuclear Reactor Instead of the Actual Two PWR: Preliminary Study - Main ResultsFribourg, C. / ASME et al. | 2002
- 601
-
GT-2002-30145 Simulation Investigation of Control Options for Full Load Rejection in the PBMR Closed Cycle Gas Turbine Power PlantBotha, B. W. / Rousseau, P. G. / ASME et al. | 2002
- 607
-
GT-2002-30146 HTGR Closed Cycle GT Plant Analysis: Options and Procedures for Startup With Hot Gas InjectionKumar, K. N. P. / Tourlidakis, A. / Pilidis, P. / ASME et al. | 2002
- 615
-
GT-2002-30147 Economic Feasibility of Fast Nuclear-Power Merchant ShipsParamonov, D. V. / ASME et al. | 2002
- 623
-
GT-2002-30148 Design and Economics of the HTGR-GT Power Plant by JAERIMuto, Y. / Ishiyama, S. / Shiozawa, S. / Tanihira, M. / Miyoshi, Y. / Ohashi, K. / ASME et al. | 2002
- 631
-
GT-2002-30149 A New Tailpipe Design for GE Frame Type Gas Turbines to Substantially Lower Pressure LossesGolomb, R. / Sahai, V. / Cheng, D. Y. / ASME et al. | 2002
- 639
-
GT-2002-30150 A New Scaling Method for Component Maps of Gas Turbine Using System IdentificationKong, C. / Ki, J. / Kang, M. / ASME et al. | 2002
- 647
-
New possibilities for combined cycles through advanced steam technologyJordal, K. / Fridh, J. / Hunyadi, L. / Jonsson, M. / Linder, U. et al. | 2002
- 647
-
GT-2002-30151 New Possibilities for Combined Cycles Through Advanced Steam TechnologyJordal, K. / Fridh, J. / Hunyadi, L. / Jonsson, M. / Linder, U. / ASME et al. | 2002
- 655
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GT-2002-30152 Universal Electric Machine for the Start-Up and Power Generation of Large Frame Size Gas TurbinesCheng, D. Y. / Nelson, A. L. C. / ASME et al. | 2002
- 663
-
GT-2002-30410 Semi-Closed Cycle O~2/CO~2 Combustion Gas Turbines: Influence of Fluid Properties on the Aerodynamic Performance of the TurbomachineryRoberts, S. K. / Sjolander, S. A. / ASME et al. | 2002
- 675
-
Exergy analysis of gas-turbine combined cycle with CO2 capture using pre-combustion decarbonization of natural gasKvamsdal, H.M. / Ertesvag, I.S. / Bolland, O. / Tolstad, T. et al. | 2002
- 675
-
GT-2002-30411 Exergy Analysis of Gas-Turbine Combined Cycle With CO~2 Capture Using Pre-Combustion Decarbonization of Natural GasKvamsdal, H. M. / Ertesvag, I. S. / Bolland, O. / Tolstad, T. / ASME et al. | 2002
- 683
-
Some unconventional aero gas turbines using hydrogen fuelBoggia, S. / Jackson, A. et al. | 2002
- 683
-
GT-2002-30412 Some Unconventional Aero Gas Turbines Using Hydrogen FuelBoggia, S. / Jackson, A. / ASME et al. | 2002
- 691
-
GT-2002-30413 The Effects of Incondensable Gases on H~2/O~2 Cycle PerformanceGambini, M. / Guizzi, G. L. / Vellini, M. / ASME et al. | 2002
- 703
-
The employment of hydrogenated fuels from natural gas reforming: gas turbine and combustion analysisBozza, F. / Cameretti, M.C. / Tuccillo, R. et al. | 2002
- 703
-
GT-2002-30414 The Employment of Hydrogenated Fuels From Natural Gas Reforming: Gas Turbine and Combustion AnalysisBozza, F. / Cameretti, M. C. / Tuccilo, R. / ASME et al. | 2002
- 715
-
Recognising the viability of cooling gas turbine inlet air in colder regions by using low pressure fogging techniquesConfurius, J. et al. | 2002
- 715
-
GT-2002-30447 Recognising the Viability of Cooling Gas Turbines Inlet Air in Colder Regions by Using Low Pressure Fogging TechniquesConfurius, J. / ASME et al. | 2002
- 721
-
GT-2002-30448 Carbon Dioxide Emission Analysis With Energy Payback EffectUtamura, M. / ASME et al. | 2002
- 729
-
GT-2002-30509 Small-Scale Well-Proven Inherently Safe Nuclear Power ConversionCrommelin, G. A. K. / ASME et al. | 2002
- 737
-
GT-2002-30510 Nuclear Gas Turbines Small-Scale Inherently Safe, Well-Proven Nuclear Powervan Dam, H. / van der Hagen, T. H. J. J. / ASME et al. | 2002
- 745
-
GT-2002-30511 Versatile Heat Source for Nuclear Gas Turbine and Hydrogen Production FacilityMcDonald, C. F. / ASME et al. | 2002
- 755
-
GT-2002-30512 ACACIA: A Small Scale Nuclear Power Plant With Cogeneration Capabilitiesvan Heek, A. I. / ASME et al. | 2002
- 763
-
GT-2002-30513 Degradation Effects on Combined Cycle Power Plant Performance: Part 3 - Gas and Steam Turbine Degradation EffectsZwebek, A. I. / Pilidis, P. / ASME et al. | 2002
- 771
-
Experimental results of hot section metal temperature measurements of Rolls-Royce Allison 501KH under massive steam injectionCheng, Dah-Yu / Nelson, A.L.C. et al. | 2002
- 771
-
GT-2002-30514 Experimental Results of Hot Section Metal Temperature Measurements of Rolls-Royce Allison 501KH Under Massive Steam InjectionCheng, D. Y. / Nelson, A. L. C. / ASME et al. | 2002
- 779
-
Cycle optimisation using an advanced, real engine performance prediction modelCoppinger, M. / Cox, G. / Hannis, J. / Cox, N. et al. | 2002
- 779
-
GT-2002-30515 Cycle Optimisation Using and Advanced, Real Engine Performance Prediction ModelCoppinger, M. / Cox, G. / Hannis, J. / Cox, N. / ASME et al. | 2002
- 789
-
GT-2002-30516 Performance Simulation of Turboprop Engine Using SIMULINK® ModelKong, C. / Roh, H. / ASME et al. | 2002
- 799
-
GT-2002-30517 Gas Properties as a Limit to Gas Turbine PerformanceWilcock, R. C. / Young, J. B. / Horlock, J. H. / ASME et al. | 2002
- 799
-
Gas properties as a limit to gas turbine performanceWilcock, R.C. / Young, J.B. / Horlock, J.H. et al. | 2002
- 809
-
GT-2002-30519 Analytical Blade Row Cooling Model for Innovative Gas Turbine Cycle Evaluations Supported by Semi-Empirical Air Cooled Blade DataTorbidoni, L. / Massardo, A. F. / ASME et al. | 2002
- 819
-
GT-2002-30550 The R-ATR and the R-REF Gas Turbine Power Cycles With CO~2 Removal: Part 2 - The R-REF CycleFiaschi, D. / Lombardi, L. / Tapinassi, L. / ASME et al. | 2002
- 827
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GT-2002-30551 Comparison of Blade Cooling Performance Using Alternative FluidsCarcasci, C. / Zecchi, S. / Oteri, G. / ASME et al. | 2002
- 835
-
GT-2002-30611 A Universal Mathematical Model for a New Combined-Cycle, Fossil-Fuel Power System (LAJ Cycle): Part 1 - Static ModelJudkins, R. R. / Armstrong, T. R. / Labinov, S. D. / ASME et al. | 2002
- 835
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A universal mathematical model for a new combined-cycle, fossil-fuel power system (LAJ cycle): Part 1 - Static modelJudkins, R.R. / Armstrong, T.R. / Labinov, S.D. et al. | 2002
- 845
-
GT-2002-30612 The LAJ Cycle: A New Combined-Cycle Fossil Fuel Power SystemJudkins, R. R. / Armstrong, T. R. / Labinov, S. D. / ASME et al. | 2002
- 845
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The LAJ cycle: A new combined-cycle fossil fuel power systemJudkins, R.R. / Armstrong, T.R. / Labinov, S.D. et al. | 2002
- 853
-
GT-2002-30647 Investigation of a Fuel Cell-Powered Blended Wing Body Airliner With Boundary Layer Re-EnergizationPachidas, V. A. / Singh, R. / ASME et al. | 2002
- 861
-
GT-2002-30649 Extrapolation of Compressor Characteristics to the Low-Speed Region for Sub-Idle Performance ModellingJones, G. / Pilidis, P. / Curnock, B. / ASME et al. | 2002
- 869
-
Feasibility and performance of an ambient pressure MCFC combined with a commercial gas turbineDesideri, U. / Lunghi, P. / Ubertini, S. et al. | 2002
- 869
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GT-2002-30650 Feasibility and Performance of an Ambient Pressure MCFC Combined With a Commercial Gas TurbineDesideri, U. / Lunghi, P. / Ubertini, S. / ASME et al. | 2002
- 877
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GT-2002-30651 A Tip-Turbine Driven Propulsion Fan ConceptCasado, H. / Cristobal, E. / Lorido, A. / Ramsden, K. W. / ASME et al. | 2002
- 877
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A tip-turbine driven propulsion fan conceptCasado, H. / Cristobal, E. / Lorido, A. / Ramsden, K.W. et al. | 2002
- 887
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Integrated micro-turbine and rotary-kiln pyrolysis system as a waste to energy solution for a small town in Central Italy - Cost positioning and global warming assessmentFantozzi, F. / Di Maria, F. / Desideri, U. et al. | 2002
- 887
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GT-2002-30652 Integrated Micro-Turbine and Rotary-Kiln Pyrolysis System as a Waste to Energy Solution for a Small Town in Central Italy: Cost Positioning and Global Warming AssessmentFantozzi, F. / Di Maria, F. / Desideri, U. / ASME et al. | 2002
- 895
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GT-2002-30653 Simplified Versus Detailed SOFC Reactor Models and Influence on the Simulation of the Design Point Performance of Hybrid SystemsMagistri, L. / Bozzo, R. / Costamagna, P. / Massardo, A. F. / ASME et al. | 2002
- 905
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GT-2002-30665 A Universal Mathematical Model for a New Combined-Cycle, Fossil-Fuel Power System (LAJ Cycle): Part 2 - Dynamic ModelJudkins, R. R. / Armstrong, T. R. / Labinov, S. D. / ASME et al. | 2002
- 905
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A universal mathematical model for a new combined-cycle, fossil-fuel power system (LAJ cycle): Part 2 - Dynamic modelJudkins, R.R. / Armstrong, T.R. / Labinov, S.D. et al. | 2002
- 913
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GT-2002-30260 United States Navy (USN) Integrated Power System (IPS) Gas Turbine Generator Set Test ExperienceHarvey, E. / Kingsley, J. / Stauffer, M. / ASME et al. | 2002
- 923
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GT-2002-30261 Rolls Royce/Allison 501-K Gas Turbine Anti-Fouling Compressor Coatings EvaluationCaguiat, D. E. / ASME et al. | 2002
- 933
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GT-2002-30262 Compressor Fouling Testing on Rolls Royce/Allison 501-K17 and General Electric LM2500 Gas TurbinesCaguiat, D. E. / Zipkin, D. M. / Patterson, J. S. / ASME et al. | 2002
- 943
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GT-2002-30263 Evaluation of at Sea Tested LM2500 Rainbow Rotor Blade CoatingsDriscoll, M. / McFetridge, E. / Arseneau, W. / ASME et al. | 2002
- 961
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GT-2002-30264 Enhanced TF40B Gas Turbine Engine Development ProgramYee, R. / Myers, L. / Braccio, K. / Dvornak, M. / ASME et al. | 2002
- 969
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GT-2002-30265 U.S. Navy Development of Air Assist Fuel Nozzle System for the 501K Series Gas Turbine EnginesHoffman, M. G. / DeCorso, R. J. / Russom, D. M. / ASME et al. | 2002
- 977
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GT-2002-30266 The WR-21 Intercooled Recuperated Gas Turbine Engine: Operation and Integration Into the Royal Navy Type 45 Destroyer Power SystemMcCarthy, S. J. / Scott, I. / ASME et al. | 2002
- 985
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GT-2002-30267 High Capacity and High Efficiency Multi-Stage Air Intake SystemHashem, A. / Fadda, D. / Fewel, K. J. / ASME et al. | 2002
- 991
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Development of the advanced cycle low-power gas turbine alternator (ACL GTA)Fielder, J. et al. | 2002
- 991
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GT-2002-30268 Development of the Advanced Cycle Low-Power Gas Turbine Alternator (ACL GTA)English, C. R. / Fielder, J. / ASME et al. | 2002
- 999
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GT-2002-30269 Through Life Management of Naval Gas Turbines for Extended Service Lives and Reduced Lifetime CostsBolwell, R. / ASME et al. | 2002
- 1013
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GT-2002-30270 Condition Monitoring and Fault Diagnosis of Naval Gas TurbinesGrzadziela, A. / Stapersma, D. / Charchalis, A. / ASME et al. | 2002
- 1025
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GT-2002-30271 Application of Diagnostic and Algorithms for Maintenance Optimization of Marine Gas TurbinesOrsagh, R. F. / Kacprzynski, G. J. / Roemer, M. J. / Scharschan, J. W. / Caguiat, D. E. / McGroarty, J. J. / ASME et al. | 2002
- 1035
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GT-2002-30272 Using a Digital Fuel Control System and Digital Engine Controller for U.S. Navy LM2500 EnginesCalabrese, M. A. / Skarbek, L. F. / Shah, P. H. / Yassine, M. K. / ASME et al. | 2002
- 1041
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GT-2002-30419 U.S. Navy Large Deck Amphibious Assault Ship: Steam to Gas Turbine ConversionHatcher, S. / Oswald, A. / Boughner, A. / ASME et al. | 2002
- 1051
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GT-2002-30673 The Design and Layout of the Propulsion Plant of the RNLN Air Defence and Command Frigate (ADCF)Broekhaus, K. O. / Rand, M. J. / ASME et al. | 2002
- 1059
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GT-2002-30675 Integrated Testing of the Full Authority Digital Control (FADC) for the U.S. Navy's CG-47 Class Ship Service Gas Turbine Generator (SSGTG) SetsConnery, B. J. / Russom, D. M. / Pineiro, I. / ASME et al. | 2002
- 1065
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GT-2002-30676 Integration of Condition Based Maintenance Technologies Into U.S. Navy Gas Turbine EnginesMcGroarty, J. J. / Scharschan, J. W. / Eghtessad, J. M. / ASME et al. | 2002
- 1073
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GT-2002-30275 Gas Turbine Performance Prediction by Using Generalized Performance Curves of Compressor and Turbine StagesSpina, P. R. / ASME et al. | 2002
- 1083
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GT-2002-30276 Gas Turbine Health Indices Determination by Using Neural NetworksBettocchi, R. / Spina, P. R. / Torella, G. / ASME et al. | 2002
- 1091
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GT-2002-30277 Measurement of Void Fraction and Pressure Drop of Air-Oil Two-Phase Flow in Horizontal PipesPawloski, J. / Ching, C. / Shoukri, M. / ASME et al. | 2002
- 1103
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GT-2002-30278 On Reducing Piping Vibration Levels: Attacking the SourceLiu, Z. / Hill, D. L. / Motriuk, R. / ASME et al. | 2002
- 1103
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On reducing piping vibration levels - attacking the sourceLiu, Zheji / Hill, D.L. / Motriuk, R. et al. | 2002
- 1111
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GT-2002-30279 Validation of Compressor Transient BehaviourBakken, L. E. / Bjorge, T. / Bradley, T. M. / Smith, N. / ASME et al. | 2002
- 1123
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GT-2002-30280 Ten Years of Industrial Gas Turbine Operating ExperiencesCowell, L. / Etheridge, C. / Smith, K. / ASME et al. | 2002
- 1123
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Ten years of DLE industrial gas turbine operating experiencesCowell, L. / Etheridge, C. / Smith, K. et al. | 2002
- 1137
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GT-2002-30281 Gas Turbine Maintenance Policy: A Statistical Methodology to Prove Interdependency Between Number of Starts and Running HoursCeschini, G. F. / Carlevaro, F. / ASME et al. | 2002
- 1143
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GT-2002-30282 Acceptance Criteria for Gas Compression SystemsKurz, R. / Fozi, A. A. / ASME et al. | 2002
- 1143
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Acceptance criteria for gas compression systemsKurz, R. / Fozi, A.A. et al. | 2002
- 1153
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GT-2002-30283 Remote Diagnostics of the Alliance Gas Pipeline System Architecture and Initial Operating ExperienceMochi, G. / Benvenuti, E. / Baldocci, R. / Bianucci, D. / ASME et al. | 2002
- 1161
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GT-2002-30538 Limits and Trade-Off in the Control of Compressor SurgeBlanchini, F. / Giannattasio, P. / Micheli, D. / Pinamonti, P. / ASME et al. | 2002
- 1173
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GT-2002-30539 A Novel Method for the Performance Modeling of a Gas Transmission CompressorPearson, W. N. / Armitage, A. F. / Henderson, D. S. / ASME et al. | 2002
- 1173
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A novel method for the performance control of a gas transmission compressorPearson, W.N. / Armitage, A.F. / Henderson, D.S. et al. | 2002
- 1185
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GT-2002-30592 Fuel System Suitability Considerations for Industrial Gas TurbinesElliott, F. G. / Kurz, R. / Etheridge, C. / O Connell, J. P. / ASME et al. | 2002
- 1185
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Fuel system suitability considerations for industrial gas turbinesElliott, F.G. / Kurz, R. / Etheridge, C. / O'Connell, J.P. et al. | 2002
- 1195
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GT-2002-30593 User Experience With P&W FT8 and GE Frame 6 Cogeneration Power PlantsHolzschuh, T. / Kovacik, M. / ASME et al. | 2002
- 1195
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User experience with P & W FT8 and GE FRAME 6 cogeneration power plantsHolzschuh, T. / Kovacik, M. et al. | 2002