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FOR A COMPLETE LISTING OF JOINT SESSIONS, SEE PAGE 32 ASME TURBO EXPO 2012 FINAL PROGRAM 55 TUESDAY, JUNE 12: 10:15 a.m. - 12:45 p.m. 10:15 10:45 11:15 11:45 12:15 CoMMITTEE: Controls, diagnostics & Instrumentation • Paper Session Room B3-M8 • TB-5-5 CoNTRoLS 1 Session Chair: Richard Meisner, Pratt & Whitney, East Hartford, CT, USA Fixed dynamic Method for Transientstate optimal Control Law design of Aircraft Engine GT2012-68837 Lei Wang, YingQing Guo, JunFeng Wu, Jun Lu, Northwestern Polytechnical University, Xi’an, shaanxi, China Study on Practical Application of Turboprop Engine Condition Monitoring and Fault diagnostic System Using Fuzzy-Neuro Algorithms GT2012-68158 Changduk Kong, Semyeong Lim, Keonwoo Kim, Chosun University, Gwangju, Korea (Republic) Reducing Conservatism in Aircraft Engine Response Using Conditionally Active Min-Max Limit Regulators GT2012-70017 Ryan May, ASRC Aerospace Corp, Cleveland, OH, USA, Sanjay Garg, NASA Glenn Research Center, Cleveland, OH, USA The Influence of Humidity on the Creep Life of A High Pressure Gas Turbine Blade: Part I Heat Transfer Model GT2012-69455 Samir Eshati, Panagiotis Laskaridis, Anthony Haslam, Pericles Pilidis, Cranfield University, Bedfordshire, UK Fuel System design for the More Electric Engine GT2012-68374 Noriko Morioka, IHI Corporation, Tokyo, Japan, Hitoshi Oyori, IHI AEROSPACE Co., Ltd., Gunma, Japan The Influence of Humidity on the Creep Life of A High Pressure Gas Turbine Blade: Part II Case Study GT2012-69462 Samir Eshati, Panagiotis Laskaridis, Anthony Haslam, Pericles Pilidis, Cranfield University, Bedfordshire, UK Flow Control over a Circular Cylinder Using Pulsed dBd Actuators GT2012-69993 William C. Schneck, III, Walter F. O’Brien, Virginia Polytechnic Institute and State University, Blacksburg, VA, USA The Balance Between Secondary Air System Pressure Head Requirements, Cooling Effectiveness And Turbine Efficiency: A Parametric Study GT2012-69896 Sergio Arias Quintero, Kaylee M. Dorman, University of Central Florida, Orlando, FL, USA, Mark Ricklick, Jayanta Kapat, Center for Advanced Turbines and Energy Research - UCF, Orlando, FL, USA An Acoustic-Based Stall-Warning System for Application In Induced-draft Boiler Fans GT2012-69050 Stefano Bianchi, Alessandro Corsini, Sapienza University of Rome, Rome, Italy, Geoff Sheard, Flakt Woods, Colchester, Essex, UK CoMMITTEE: Cycle Innovations • Paper Session Room 18 • TB-6-6 CyCLE PERFoRMANCE ANd HEALTH Session Chair: Alberto Traverso, University of Genoa, Genova, Italy • Session Co-Chair: Alessandro Sorce, University of Genoa, Genova, Italy design and Analysis of Volute Casing: A Review GT2012-68056 Beena Baloni, Salim Channiwala, Sardar Vallabhbhai National Institute of Technology, Surat, Surat, India Theoretical Interpretation of the CoRdIER-Lines for Squirrel-Cage and Cross-Flow Fans GT2012-68186 Reinhard Willinger, Vienna University of Technology, Vienna, Austria Sirocco Fan design for Residential Ventilation through Multi-objective optimization to Enhance Aerodynamic Performance GT2012-68528 Jin-Hyuk Kim, Kyung-Hun Cha, Kwang-Yong Kim, Inha University, Incheon, Korea (Republic) System Matched 3d Radial Impeller design with Variable Inlet Angle distributions GT2012-70024 Matthias Semel, Henrik Smith, Philipp Epple, Oliver Litfin, Antonio Delgado, University of Erlangen, Erlangen, Germany, Klaus Pfannschmidt, Detlev Grobeis, actiro GmbH & Co. KG, Suhl, Germany Performance Evaluation of a 5kN Gas Turbine based on Specially design Components GT2012-70020 Jesuíno Takachi Tomita, Cleverson Bringhenti, Joao Roberto Barbosa, Vitor Alexandre Carlesse Martins, Instituto Tecnológico de Aeronáutica - ITA, São José dos Campos, Sao Paulo, Brazil CoMMITTEE: Fans & Blowers • Paper Session Room B3-M6 • TB-9-4 CENTRIFUGAL FANS Session Chair: guang xi, Xi’an Jiaotong Univ, xi’an, Shaanxi, China • Session Co-Chair: Hua Chen, Honeywell UK Ltd., Chesire, UK
Look for this Symbol R for Gas Turbine User Related Sessions ASME TURBO EXPO 2012 FINAL PROGRAM 56 TUESDAY, JUNE 12: 10:15 a.m. - 12:45 p.m. 10:15 10:45 11:15 11:45 12:15 CoMMITTEE: Heat Transfer: General Interest • Paper Session Room B4-M12 • TB-10-10 EFFECTS oF RoTATIoN oN INTERNAL HEAT TRANSFER Session Chair: Tong Miin Liou, National Tsing Hua University, Hsinchu, Taiwan • Session Co-Chair: Michael Barringer, The Pennsylvania State University, University Park, PA, USA Effects of Rotation and Channel orientation on the Flow Field Inside a Trailing Edge Internal Cooling Channel GT2012-68050 Matteo Pascotto, Alessandro Armellini, Luca Casarsa, Pietro Giannattasio, Claudio Mucignat, University of Udine, Udine, Italy CoMMITTEE: Heat Transfer: Film Cooling • Paper Session Room B4-M10 • TB-11-11 GENERAL FILM CooLING II Session Chair: Ardy Riahi, Honeywell, Phoenix, AZ, USA • Session Co-Chair: John Clark, Air Force Research Laboratory, Wright-Patterson AFB, OH, USA determination of Time-Resolved Heat Transfer Coefficient and Adiabatic Effectiveness Waveforms with Unsteady Film Cooling GT2012-68652 James Rutledge, Jonathan F. McCall, Air Force Institute of Technology, Wright- Patterson AFB, OH, USA, Emergence of Kelvin-Helmholtz Instabilities in Gas Turbine Rim Cavities A Parameter Study GT2012-68834 Michael Rabs, Friedrich Benra, University of Duisburg-Essen, Duisburg, Germany, Oliver Schneider, Siemens AG- Energy Sector, Mülheim, Germany Effect of Channel orientation In A Rotating Wedge-shaped Cooling Channel With Pin Fins And Ribs GT2012-68439 Lu Qiu, Hongwu Deng, Zhi Tao, Beihang University, Beijing, Beijing, China Effect of Upstream Wake on Passage Flow and Tip Film Cooling Characteristics GT2012-68562 Jin Wang, Xi’an Jiaotong University, Xi’an, China, Bengt Sunden, Lund university, Lund, Sweden, Min Zeng, Qiuwang Wang, Xi’an Jiaotong University, Xi’an, China Experimental Measurements of Ingestion Through Turbine Rim Seals. Part 3: Single and double Seals GT2012-68493 Carl Sangan, Oliver Pountney, James Scobie, Mike Wilson, Mike Owen, Gary Lock, University of Bath, Bath, UK Experimental Survey on Heat Transfer In A Trailing Edge Cooling System: Effects of Rotation In Internal Cooling ducts GT2012-69638 Leonardo Bonanni, Università di Firenze, Firenze, Italy, Carlo Carcasci, Bruno Facchini, Lorenzo Tarchi, University of Florence, Florence, Italy Influence of Passage Flow on Tip Film Cooling Characteristics GT2012-68563 Jin Wang, Yong Yu, Min Zeng, Qiuwang Wang, Xi’an Jiaotong University, Xi’an, China Method for 1-d Rotating/Stationary disk Cavity Heat Transfer Analysis with Partial Flow Ingestion in a Gas Turbine GT2012-68295 Kuo-Ting Hsia, Chad Garner, Gregory Vogel, PSM - An ALSTOM company, Jupiter, FL, USA Unsteady CFd Analysis of Turbulent Flow and Heat Transfer in a Gas Turbine Blade Trailing Edge Subjected to Rotation GT2012-69903 Domenico Borello, Sapienza University Of Rome, Rome, Italy, Giovanni Delibra, Dept. of Mechanical and Aerospace Engineering, Sapienza University of Rome, Roma, Italy, Cosimo Bianchini, Antonio Andreini, University of Florence, Florence, Italy Second Law Analysis of Aerodynamic Losses: Results for a Cambered Vane With and Without Film Cooling GT2012-70021 Philip Ligrani, Jae Sik Jin, Saint Louis University, St. Louis, MO, USA Computational Extrapolation of Turbine Sealing Effectiveness from Test Rig to Engine Conditions GT2012-68490 Roy Teuber, Mike Wilson, Gary Lock, Mike Owen, University of Bath, Bath, UK, Yan Sheng Li, John Maltson, Siemens Industrial Turbomachinery Ltd., Lincoln, UK Passive Effusion Cooling in an S-Bend diffuser GT2012-68560 Billy CN Ng, A. Michael Birk, Queen’s University, Kingston, ON, Canada CoMMITTEE: Heat Transfer: Internal Air Systems and Seals (with Turbomachinery) • Paper Session Room B4-M14 • TB-12-3 RoToR-STAToR CAVITIES 2 Session Chair: Bruce Johnson, Pratt & Whitney/Independent Contractor, Manchester, CT, USA • Session Co-Chair: Cheng-Zhang Wang, Pratt and Whitney, East Hartford, CT, USA, Peter Childs, Imperial College London, London, UK Effect of Ingestion on Heat Transfer to Turbine discs GT2012-68496 Oliver Pountney, Carl Sangan, Mike Owen, Gary Lock, University of Bath, Bath, UK
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134 IGTI Board ASME Vice President,
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Saturday, June 9 144 Turbo Expo 201
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