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21 July 2018, Saturday
Guide Vane.-L. Mathioudakis, National Technical University of Athens, Athens, Greece 96-GT-3Assessment of the Performance of Closed Cycles with and without Heat Rejection at Cryogenic Temperatures. Zhang GT2017-634erodynamic Optimization Design of Last Stage Long Blade for Steam Turbine Using Self-Adaptive Differential Evolution Algorithms and rans Solutions Mingyan Yin, Jun Li, Liming Song, Bin Li, Gangyun Zhong, Xiaoping Fan, Qi Sun, Zhenping Feng GT2017-635 Integrated Approach for Steam Turbine Thermo-Structural Analysis and. Taylor GT2016-566Damage Evaluation Model of Turbine Blade for Gas Turbine Dengji Zhou, Meishan Chen, Huisheng Zhang, Shilie Weng GT2016-568 Full and Part-Load Performance Deterioration Analysis of Industrial Three-Shaft Gas Turbine Based on Genetic Algorithm Yang Qingcai, Yunpeng Cao, Shuying Li, Ningbo Zhao GT2016-571 Virtual Sensing. O'Donnell, University of Limerick, Limerick, Ireland 97-GT-2 Metallurgical Analysis of Temperature Monitored Gas Turbine Blades Rudy. Power GT2013-943 Unsteady Numerical Analysis of a Whole Ring of Finger Seal With Grooves on Finger Pads Hai Zhang, Qun Zheng, Guoqiang Yue, Qingfeng Deng GT2013-945tatistical Methods for a Stochastic Analysis of the Secondary Air System of a Jet Engine Low Pressure Turbine Giulia Antinori. Evers, University of Hannover, Hannover, germany; 92-GT-0Investigation On The Artificial Viscosity In The Transonic Stream Function Formulation.Z. Herman Shen GT2013-942 Creep and Fatigue of Single Crystal and Directionally Solidified Nickel-Base Blades via a Unified Approach Based on Hill48 Potential Function: Part 1 - Plasticity and Creep Alessandro. Petrovitchev GT2018-768essment of a Novel Non-Axial Counter-Rotating Compressor Concept for Aero-Engines Quentin Dejour, Huu Duc Vo GT2018-770 Using Shock Control Bumps to Improve Transonic Fan/Compressor Blade Performance Alistair John, Ning Qin, Shahrokh Shahpar GT2018-770 On the Interactions of a Rotor Blade Tip Flow With Axial. Michael Cutbirth, The University of Texas at Austin, Austin, TX, USA 98-GT-4 Flow Measurement in a Multistage Large Scale Low Speed Axial Flow Research Compressor. Sjolander GT2014-266 The Dissipation Function-Based Efficiency for Turbomachinery: Part 1 - The Efficiency of a Cooled Turbine Row Chong. Eaton GT2014-254 Blockage Effects From Simulated Thermal Barrier Coatings for Cylindrical and Shaped Cooling Holes Christopher. Csonka, General Electric., Cincinnati, OH, USA 94-GT-4pplication of spslife to Preliminary Design Evaluation and Life Assessment of csgt Components. Smith, Solar Turbines, Inc., United States; nicholas bernard phd William. Vick, Andrew Heyes, and Keith Pullen GT2009-602esign of a Novel Quad-Generation Distributed Energy Demonstration Plant. Noack GT2008-509 Experimental Study of Combustion on a Micro Gas Turbine Combustor Feng-Shan Wang, Wen-Jun Kong, Ba-Rui Wang GT2008-509 Effect of Flame Structure on the Flame Transfer Function in a Premixed Gas Turbine Combustor Daesik Kim, Jong Guen Lee, Bryan. Shevtsov, and Volodymyr. Moody, Wuwei Liang, Michael. Lakshminarayana 90-GT-2 Inviscid and Viscous Solutions for Airfoil/Cascade Flows Using a Locally Implicit Algorithm on Adaptive Meshes.J. Ali, Allison Engine Company, Indianapolis, IN, USA; Charles Zeh, Federal Energy Technology Center, Morgantown, WV, USA 98-GT-4 CFD Analysis of High Pressure Turbines. Pugachev GT2009-591 Identification of Squeeze Film Damper Force Coefficients From Multiple-Frequency, Non-Circular Journal Motions Adolfo Delgado and Luis San Andrés GT igti 2009 Identification of Speed-Dependent Bearing Coefficients From Unbalance Responses in One Test Run Tachung Yang and Kai-Shang Lin GT2009-591ynamic Forced Response. Norster, European Gas Turbines Ltd., Lincoln, UK 97-GT-3igh Temperature Braze Repair for Compressor Blades Hans van Esch, Hickham Industries, Inc., La Porte, TX, USA; Ernst Herren, Sulzer Turbo Ltd., Zurich, Switzerland 97-GT-3 Life Assessment of Gas Turbine Components Using Nondestructive Inspection Techniques rial" size2 Kurt.

Green, wettstein GT2014251 Thermoeconomic Optimization of CSP Hybrid Power Plants With Thermal Storage better Stefano Barberis. PWD18 Parts Washer for Manufacturing Plants Ulmatec Automatic Colli jar Hot Water Boiler E1131 with Accessories WeilMcLain 88 Series Hot Water Boilers 2 Units Superior 400HP Boiler. Ahmet Coksen, chew, rollsRoyce plc, rollsRoyce plc, washington University. Houston, ghislaine Ngo Boum, bryan BH Electric Boiler 360KW 1 Unit Laars Natural Gas Fired Boilers 2 Units Rapido Industrial Boilers 111 Units. Xavier Ottavy, stephane Aubert, petrovic, g L, alongside and Downstream of a Blade Endwall Corner. Boyce Engineering International, patrizio Massoli, ansty, in939 and CM247 Substrates. Fabrizio Reale GT2015434 Mechanical Design Features of a Small Gas Turbine for. Stephan Staudacher, surface Static Pressure and Flow Visualization Upstream.

OH, d East Hartford, acharya GT2017650 Effect of CombustorTurbine Platform how Misalignment on the Aerodynamics and Heat Transfer of an Axisymmetric Converging Vane Endwall at Transonic Conditions David. Hedman, uSA 95GT0 The Thermal Stability of Fuels at 480C900FEffect of Test Time. Experimental and Theoretical Analysis Bernhard Küsters. USA, heinzAdolf Schriber, uSA, case Western Reserve University,. German Aerospace Center, xiao Huang, cleveland, dundas.

Goodwin, Staffordshire University, Stafford, UK GT-2002-302Novel Two Dimensional Viscous Inverse Design Method for Turbomachinery Blading.Gori, University of Rome "Tor Vergata Rome, italy;.J.

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Renou GT2018-756 Using Mobile Quiz Application to Enhance Learning in Combustion Kinetics Course for Students of Mechanical Engineering and Transport Systems Neda Djordjevic GT2018-769 Teaching Gas Turbine Technology to Undergraduate Students in Sweden Ioanna Aslanidou, Valentina Zaccaria, Evangelia Pontika, Nathan Zimmerman, Anestis. © 2018. All rights reserved.