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Look for this symbol ✲ for Gas Turbine user related sessions. FINAL PROGRAM TURBO EXPO 2010 • 44 MONDAY, JUNE 14: 2:30 p.m. – 5:30 p.m. 2:30 3:00 3:30 4:00 4:30 5:00 COMMITTEE: Heat Transfer: Film Cooling • Paper Session Room: Alsh 2 • SECC • MB-10-2 ENDWALL FILM COOLING Session Chair: Ardy Riahi, Honeywell Int., Phoenix, AZ, USA Session Co-Chair: James Heidmann, NASA Glenn Research Center, Cleveland, OH, USA Effects of an Axisymmetric Contoured Endwall on a Nozzle Guide Vane: Adibatic Effectiveness Measurements GT2010-22968 Alan Thrift, Karen A. Thole, The Pennsylvania State University, University Park, PA, USA, Satoshi Hada, Mitsubishi Heavy Industries, LTD, Takasago, Hyogo, Japan Effects of an Axisymmetric Contoured Endwall on a Nozzle Guide Vane: Heat Transfer Measurements GT2010-22970 Alan Thrift, Karen A. Thole, The Pennsylvania State University, University Park, PA, USA, Satoshi Hada, Mitsubishi Heavy Industries, LTD, Takasago, Hyogo, Japan Computational Predictions of Heat Transfer and Film- Cooling for a Turbine Blade with Non-Axisymmetric Endwall Contouring GT2010-22984 Stephen Lynch, Virginia Tech, Blacksburg, VA,USA, Karen A. Thole, The Pennsylvania State University, University Park, PA, USA, Atul Kohli, Pratt & Whitney, East Hartford, CT, USA, Christopher Lehane, United Technologies– Pratt & Whitney, East Hartford, CT, USA The Role of Density Ratio and Blowing Ratio on Film Cooling in a Vane Passage GT2010-23680 James Post, Sumanta Acharya, Louisiana State University, Baton Rouge, LA, USA Endwall Effusion Cooling System Behaviour Within a High-Pressure Turbine Cascade. Part 1: Aerodynamic Measurements GT2010-22931 Daniele Simoni, Università degli Studi di Genova, Genova, Italy, Marina Ubaldi, Pietro Zunino, Marco Sacchi, Università di Genova, Genova, Italy, Stefano Zecchi, AVIO S.P.A., Torino, Italy Endwall Effusion Cooling System Behaviour Within a High-Pressure Turbine Cascade. Part 2: Heat Transfer and Effectiveness Measurements GT2010-22932 Lorenzo Tarchi, University of Florence, Firenze,Italy, Bruno Facchini, Dipartimento di Energetica S.Stecco - University of Florence, Florence, Italy, Stefano Zecchi, AVIO S.P.A., Torino, Italy, Lorenzo Toni, University of Florence, Firenze, Italy COMMITTEE: Heat Transfer: Internal Air and Seals (with Turbomachinery Committee) • Paper Session Room: Boisdale 1 • SECC • MB-11-3 RIM SEALING Session Chair: Axel Glahn, Pratt & Whitney, East Hartford, CT, USA Session Co-Chair: John Chew, University of Surrey, Guildford, Surrey, UK Aerothermal Impact of the Interaction between Hub Leakage and Mainstream Flows in Highly-Loaded HP Turbine Blades GT2010-22311 Ivan Popovic, Howard Hodson, University of Cambridge, Cambridge,UK Theoretical Prediction of Ingress through Turbine Rim Seals. Part 1: Externally- Induced Ingress GT2010-23346 Mike Owen, Oliver Pountney, Gary Lock, Mike Wilson, Kunyuan ZHOU, University of Bath, Bath,UK Theoretical Prediction of Ingress through Turbine Rim Seals. Part 2: Combined Ingress GT2010-23349 Mike Owen, Oliver Pountney, Gary Lock, University of Bath, Bath,UK Parametric Single Gap Turbine Rim Seal Model With Boundary Generation For Asymmetric External Flow GT2010-22434 Marcus Huening, Private Author, Blankenfelde- Mahlow,Germany Large-Eddy Simulation of Turbine Rim Seal Ingestion GT2010-22962 Thomas S. D. O’Mahoney, Nicholas J. Hills, John Chew, University of Surrey, Guildford,UK, Timothy Scanlon, Rolls-Royce plc, Derby,UK Investigation of Augmented Angel Wing Sealing Through the Use of Surface Concavity Arrays GT2010-22775 Ronald Bunker, Nuo Sheng, GE Global Research, Niskayuna, NY,USA COMMITTEE: Manufacturing Materials & Metallurgy • Panel Session Room: Hall 1 • SECC • MB-15-6 DESIGN, MANUFACTURING AND REPAIR OF COMBUSTION COMPONENTS Session Chair: Douglas R Nagy, Liburdi Turbine Services, Dundas, Canada Design and operating experience with fuel flexible syngas burners Federico Bonzani, Ansaldo Energia, Genova,Italy The Design, Evaluation, and Lifing of Combustor System Materials from a Honeywell Aerospace Perspective Benjamin Peterson, PhD, Honeywell Aerospace, Phoenix, AZ,USA Advanced Repair Processes for Gas Turbine Combustion Hardware John Bottoms, Liburdi Turbine Services, Mooresville,USA ✲
For a complete listing of Joint Sessions please see page 34 FINAL PROGRAM TURBO EXPO 2010 • 45 MONDAY, JUNE 14: 2:30 p.m. – 5:30 p.m. 2:30 3:00 3:30 4:00 4:30 5:00 COMMITTEE: Microturbines & Small Turbomachinery • Paper Session Room: Dochart 1 • SECC • MB-17-1 HEAT EXCHANGERS DESIGN & OPTIMIZATION Session Chair: Wendy J. Matthews, Capstone Turbine Corporation, Chatsworth, CA, USA Recent advances in High Temperature Ceramic Regenerators for Externally Fired Gas Turbines. Theoretical and experimental results GT2010-23806 Jon Huete, Alfonso Acuñas, Ibon Amallobieta, Pigmaly, Zamudio, Spain A high-efficiency heat exchanger for closed cycle and heat recovery gas turbines GT2010-22509 Luciano Andrea Catalano, Fabio De Bellis, Riccardo Amirante, Matteo Rignanese, Polytechnic of Bari, Bari, Italy Experimental Investigation of the Dynamic Performance of a Micro Gas Turbine Recuperator Including Innovative Cycle Configurations GT2010-22299 Mario Ferrari, Alessandro Sorce, Matteo Pascenti, Aristide F. Massardo, University of Genoa, Genova, Italy Modeling an installation of recuperative heat exchangers for an aero engine GT2010-22263 Dimitrios Missirlis, Kyros Yakinthos, Apostolos Goulas, Laboratory of Fluid Mechanics and Turbomachinery, Aristotle University of Thessaloniki, Thessaloniki, Greece, Olivier Seite, MTU Aero Engines GmbH, Munchen, Germany Numerical Study of Internally Finned Bayonet Tubes in a High Temperature Bayonet Tube Heat Exchanger with Inner and Outer fins GT2010-22360 Ting Ma, Mei Lin, Min Zeng, Yanpeng Ji, Qiuwang Wang, Xi’an Jiaotong University, Xi’an, Shaanxi, China COMMITTEE: Microturbines & Small Turbomachinery • Paper Session Room: Dochart 2 • SECC • MB-17-2 ROTATING COMPONENTS I: BEARINGS & ROTORDYNAMICS Session Chair: Dan Lubell, Capstone Turbine Corp., Chatsworth, CA, USA Remaining Technical Challenges and Future Plans For Oil-Free Turbomachinery GT2010-22086 Christopher DellaCorte, Robert Bruckner, NASA Glenn Research Center, Cleveland, OH, USA Evolutionary Optimization of Micro- Thrust Bearings with Periodic Partial Trapezoidal Surface Texturing GT2010-22495 Christos I. Papadopoulos, Lambros Kaiktsis, National Technical University of Athens, Dept. of Naval Architecture & Marine Engineering, Zografou, Greece, Pantelis, G Nikolakopoulos, Department of Mechanical Engineering & Aeronautics, University of Patras, Patras, Greece On the Development of An Oil-Free, High-Speed and High-Temperature Turboalternator GT2010-22852 Hooshang Heshmat, James F. Walton II, Mohawk Innovative Technology, Inc., Albany, NY, USA Development of a High Speed Gas Bearing Test Rig to Measure Rotordynamic Force Coefficients GT2010-23217 Jeffrey Moore, Andrew Lerche, David Ransom, Timothy C. Allison, Southwest Research Institute, San Antonio, TX, USA, Dan Lubell, Capstone Turbine Corp., Chatsworth, CA,USA
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REGISTRATION HOURS Sunday, June 13
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Committee Point Contacts & Vanguard
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HEAT TRANSFER Richard B. Rivir AFRL
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ASME International Gas Turbine Inst
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