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Look for this Symbol R for Gas Turbine User Related Sessions ASME TURBO EXPO 2011 FINAL PROGRAM 74 TUESDAY, JUNE 7: 2:30 p.m. - 5:00 p.m. 2:30 3:00 3:30 4:00 4:30 COMMITTEE: Turbomachinery: Axial Fan & Compressor Aerodynamics • Paper Session Room 116/117 • TC-29-3 CORNER StAll, DUCt DESigN Session Chair: Nick Nolcheff, Honeywell, Phoenix, AZ, USA • Session Co-Chair: Rudolf Selmeier, GE Global Research, Garching / Munich, Germany Experimental investigations of Corner Stall in a linear Compressor Cascade GT2011-45236 Wei Ma, Ecole Centrale de Lyon, Lyon, France, Xavier Ottavy, Ecole Centrale de Lyon, Ecully, France (Metro), Lu Lipeng, Beijing University of Aeronautics and Aerospace, Beijing, China, Leboeuf Francis, Ecole Centrale de Lyon, Ecully, France (Metro), Gao Feng, Beijing University of Aeronautics and Aerospace, Beijing, China COMMITTEE: Turbomachinery: Axial Turbine Aerodynamics • Paper Session Room 212 • TC-30-5 tURBiNE AERODyNAMiC DESigN & MODEliNg Session Chair: yavuz guendogdu, MTU Aero Engines GmbH, München, Germany • Session Co-Chair: Dragan Kozulovic, Technische Universität Braunschweig, Braunschweig, Germany Roughness Modeling for turbomachinery GT2011-45424 Andreas Fiala, MTU Aero Engines GmbH, Munich, Germany, Edmund Kuegeler, German Aerospace Center (DLR), Cologne, Germany integrated OgV Design for an Aggressive S-Shaped Compressor transition Duct GT2011-45627 A Duncan Walker, Ashley G Barker, Jon F. Carrotte, Loughborough University, Loughborough, Leicestershire, UK, John J Bolger, Matthew Green, Rolls-Royce plc, Derby, UK Anisotropic Eddy Viscosity in the Secondary Flow of a low-Speed linear turbine Cascade GT2011-45578 Gordon MacIsaac, Carleton University, Ottawa, ON, Canada, Steen Sjolander, Carleton University, Ottawwa, ON, Canada Numerical Design and Experimental Evaluation of an Aggressive S-Shaped Compressor transition Duct with Bleed GT2011-45628 A Duncan Walker, Ashley G Barker, Jon F. Carrotte, Loughborough University, Loughborough, Leicestershire, UK influence of Surface Roughness On the Profile And End-wall losses in low Pressure turbines GT2011-46371 Raul Vazquez, Industria de Turbopropulsores S.A. (ITP), San Fernando de Henares, Madrid, Spain, Diego Torre, Industria de Turbopropulsores S.A (ITP), San Fernando de Henares, Madrid, Spain, Fernando Partida-Santos, CTA, Zamudio, Bizkaia, Spain, Leyre Armañanzas, ITP, San Fernando de Henares, Madrid, Spain, Antonio Antoranz, ITP, Madrid, Spain investigations of Secondary Flow Suction in a High Speed Compressor Cascade GT2011-46479 Christoph Gmelin, Technische Universitaet Berlin, Berlin, Germany, Karsten Liesner, Robert Meyer, German Aerospace Center (DLR), Berlin, Germany, Frank Thiele, Technische Universitaet Berlin, Berlin, Berlin, Germany Numerical Analysis Of three- Dimensional turbine Airfoil Designs GT2011-46204 Thorsten Poehler, RWTH Aachen University, Aachen, NRW, Germany, Yavuz Guendogdu, MTU Aero Engines GmbH, München, Germany, Jochen Gier, MTU Aero Engines, Muenchen, Germany, Peter Jeschke, Institute of Jet Propulsion and Turbomachinery RWTH Aachen, Aachen, Germany A Preliminary Numerical Cfd Analysis Of transonic Compressor Rotors When Subjected to inlet Swirl Distortion GT2011-46560 Javier C. Montes, Ahad Mehdi, Domenico D. Cugno, Vassilios Pachidis, Cranfield University, Cranfield, UK Further investigation of the influence of Real-World Blade Profile Variation on the Aerodynamic Performance of transonic Nozzle guide Vanes GT2011-46558 Jordan Ilott, Asad Asghar, William Allan, Royal Military College of Canada, Kingston, ON, Canada, Ray Woodason, StandardAero Ltd, Winnipeg, MB, Canada
FOR A COMPLETE LISTING OF JOINT SESSIONS, SEE PAGE 34 ASME TURBO EXPO 2011 FINAL PROGRAM 75 TUESDAY, JUNE 7: 2:30 p.m. - 5:00 p.m. 2:30 3:00 3:30 4:00 4:30 COMMITTEE: Turbomachinery: Radial Turbomachinery • Paper Session Room 210 • TC-33-9 CENtRiFUgAl COMPRESSORS - DESigN AND OPtiMiZAtiON Session Chair: greg Holbrook, Honeywell International, Phoenix, AZ, USA • Session Co-Chair: Subenuka Sivagnanasundaram, Queen’s University Belfast, Belfasts, Northern Ireland, UK An Optimization Procedure for the Aerodynamic Model tuning of Centrifugal Compressor Stages GT2011-45499 Susanne Svensdotter, GE Oil&Gas, France, Le Creusot, France (Metro), Omar El Shamy, GE Oil&Gas, Doha, Qatar, Nidal Ghizawi, GE Global Research, Doha, Qatar, Vittorio Michelassi, GE Oil&Gas, Florence, Italy, Sivasubramaniyan Sankaran, General Electric, Bangalore, Karnataka, India COMMITTEE: Turbomachinery: Unsteady Flows in Turbomachinery • Paper Session Room 222 • TC-34-1 StAll/SURgE i Session Chair: yuan Dong Surge inception in a transonic Centrifugal Compressor Stage GT2011-45116 Isabelle Trebinjac, Ecole Centrale de Lyon, Ecully, France (Metro), Nicolas Bulot, Turbomeca, Bordes, France (Metro), Xavier Ottavy, Nicolas Buffaz, Ecole Centrale de Lyon, Ecully, France (Metro) Blade Section Modeling and Design Dewey Hodges, Georgia Tech, Atlanta, USA Optimization of 6.2:1 pressure ratio centrifugal compressor impeller by 3D inverse design GT2011-46505 Mehrdad Zangeneh, University College London, London, Uk, Nuno Amarel, Kasra Daneshkhah, Advanced Design Technology, London, Uk, Hartmut Krain, Krain Consultancy, Neunkirchen- Seelscheid, Germany Rotor tip Flow-Field near inception Point of Rotating instability in an Axial-Flow Fan GT2011-45338 Takahiro Nishioka, Toshio Kanno, Hitachi Plant Technologies, Ltd., Ibaraki, Japan, Kiyotaka Hiradate, Mechanical Engineerign Research Laboratory, Hitachi, Ltd, Hitachinaka, Ibaraki, Japan Wind turbine Manufacturing Advancements for large Wind turbines Amir Mikhail, Clipper Wind, Santa Barbara, USA Annular Cascade for Radial Compressor Development GT2011-46834 Christian Aalburg, Ismail Sezal, Christian Haigermoser, Alexander Simpson, GE Global Research, Garching b. München, Bavaria, Germany, Vittorio Michelassi, Giuseppe Sassanelli, GE Oil&Gas, Florence, Italy Stall Warning By Blade Pressure Signature Analysis GT2011-45850 Anna Young, Ivor Day, Whittle Laboratory, University of Cambridge, Cambridge, UK, Graham Pullan, University of Cambridge, Cambridge, UK Wind turbine Manufacturing: gE Perspective Stephen Johnson, GE, Greenville, USA Assessment Of Various turbulence Models in A High Pressure Ratio Centrifugal Compressor With An Object Oriented Cfd Code GT2011-46829 Luca Mangani, Hochschule Luzern Technik& Architektur, Horw, Switzerland, Ernesto Casartelli, Hochschule Luzern - Technik & Architektur, Horw, Switzerland, Sebastiano Mauri, MAN Diesel & Turbo Schweiz AG, Zurich, Switzerland Validation Of Numerical Simulation For Rotating Stall in A transonic Fan GT2011-46109 Minsuk Choi, Imperial College London, London, UK, Nigel H. S. Smith, Rolls-Royce PLC, Derby, UK, Mehdi Vahdati, Imperial College London, London, UK Active Rotor Concepts Brain Wake, United Technologies Research Center, East Hartford, US A Method to Calculate the Performance Map Of A Centrifugal Compressor Stage GT2011-45502 Michael Casey, Universität Stuttgart, Stuttgart, Germany, Chris Robinson, PCA Engineers Ltd., Lincoln, UK A Summary of Stall Warning and Suppression Research with Micro tip injection GT2011-46118 Lin Feng, Tong Zhiting, Institute Of Engineering Thermophysics Chinese Academy Of Sciences, Beijing, China, Shaojuan Geng, Jingxuan Zhang, Jingyi Chen, Chaoqun Nie, Chinese Academy Of Sciences, Beijing, China COMMITTEE: Wind Turbine Technology • Panel Session Room 215/216 • TC-37-8 WiND tURBiNE MANUFACtURiNg ADVANCEMENtS Session Chair: lakshmi Sankar, Georgia Institute of Technology, Atlanta, GA, USA 8 Session Co-Chair: Harold Simmons, Southwest Research Institute, San Antonio, TX, USA R
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Dear Turbo Expo 2011 Participants:
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4 grand Opening Featuring Keynote S
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6 Networking Events grand Opening M
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8 Participating Organizations ASME
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10 guest Tours Vancouver City Tour
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12 Facility Tours Take advantage of
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14 Session Participant Information
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16 Exhibit Hall Floor Plan Subject
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18 Exhibitor Booth listings ADvAnCE
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20 Exhibitor Booth listings COnCEPT
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22 Exhibitor Booth listings iMPACT
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FOR A COMPLETE LISTING OF JOINT SES
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FOR A COMPLETE LISTING OF JOINT SES
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REGISTRATION HOURS Sunday, June 5 .
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Committee Point Contacts & Vanguard
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INDUSTRIAL & COGENERATION Qun Zheng
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ASME International Gas Turbine Inst
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Corporan, E. ......................
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Li, Z. ............................
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Storer, J. ........................
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The Most Important Conference for T
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