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FOR A COMPLETE LISTING OF JOINT SESSIONS, SEE PAGE 32 ASME TURBO EXPO 2012 FINAL PROGRAM 123 FRIDAY JUNE 15: 10:15 a.m. - 12:45 p.m. 10:15 10:45 11:15 11:45 12:15 COMMITTEE: Turbomachinery: Axial Flow Fan & Compressor Aerodynamics • Paper Session Room 20 • FB-33-4 dESIgn, AnAlySIS, And TEST IV Session Chair: Kwang-yong Kim, Inha University, Incheon, Korea (Republic) • Session Co-Chair: JaeHo Choi, Samsung Techwin, Seongnam, Gyeonggi, Korea (Republic) design Of Compressor Blades Considering Efficiency And Stability using CFd Based Optimization GT2012-69272 Lars Ellbrant, Lars-Erik Eriksson, Chalmers University of Technology, Gothenburg, Sweden, Hans Mårtensson, Volvo Aero Corporation, Trollhättan, Sweden A Multi-objective Constrained Aeromechanical Optimization of an Axial Compressor Transonic Blade GT2012-68993 Andrea Silingardi, Pio Astrua, Stefano Piola, Federico Bonzani, Ansaldo Energia, GENOA, Italy Multi disciplinary design Optimization and Performance Evaluation of a Single- Stage Transonic Axial Compressor GT2012-69252 Young Seok Kang, Tae Choon Park, Soo Seok Yang, Korea Aerospace Rsearch Institute, Daejeon, Korea (Republic), Sae Il Lee, Graduate School of Seoul National University, Seoul, Korea (Republic), Dong Ho Lee, Seoul National University, Seoul, Korea (Republic) Three-dimensional Flow Through a Compressor Cascade with Circulation Control GT2012-68593 Susanne Fischer, Lars Mueller, Technische Universitaet Braunschweig, Braunschweig, Germany, Horst Saathoff, Siemens AG, Energy Sector, Muehlheim an der Ruhr, Germany, Dragan Kozulovic, Technische Universitaet Braunschweig, Braunschweig, Germany development and Applications of a Stage Stacking Procedure GT2012-69115 Sameer Kulkarni, Mark Celestina, John J. Adamczyk, NASA Glenn Research Center, Cleveland, OH, USA COMMITTEE: Turbomachinery: Axial Flow Fan & Compressor Aerodynamics • Paper Session Room BV1 • FB-33-7 FlOW COnTROl Session Chair: Paolo gaetani, Politecnico di Milano, Milano, Italy • Session Co-Chair: Jean francois Brouckaert, von Karman Institute for Fluid Dynamics, Rhode-Saint-Genese, Belgium Experimental and numerical Study of a Subsonic Aspirated Cascade GT2012-69011 Antoine Godard, Ecole Centrale de Lyon - LMFA, Ecully Cedex, France, François Bario, CNRS - LMFA, Ecully Cedex, France, Stephane Burguburu, Office National d’Etudes et de Recherches Aérospatiales, Meudon, France, Francis Leboeuf, Ecole Centrale de Lyon - LMFA, Ecully Cedex, France High Pressure Compressor Stabilization by Controlled Pulsed Injection GT2012-68460 Sven-Jürgen Hiller, MTU Aeroengines GmbH, München, Germany, Jakob Hermann, Robert Widhopf-Fenk, IfTA Ingenieurbüro für Thermoakustik GmbH, Gröbenzell, Germany Corner Separation Control in a Highly loaded Compressor Cascade using Plasma Aerodynamic Actuation GT2012-69196 Yun Wu, Air Force Engineering University of PRC, Xi’an, Shaanxi, China, Xiao-hu Zhao, Ying-hong Li, Air Force Engineering University, Xi’an, Shaanxi, China, Jun Li, Air Force Engineering University of PRC, Xi’an, Shaanxi, China On the use of Synthetic Jets in Transonic Compressors GT2012-69476 Roberto Biollo, Emanuele Staffieri, ernesto benini, University of Padova, Padova, Italy Active Flow Control Techniques on a Stator Compressor Cascade: A Comparison Between Synthetic Jet and Plasma Actuators GT2012-69535 Maria Grazia De Giorgi, Stefania Traficante, Carla G. De Luca, Daniela Bello, Antonio Ficarella, University of Salento, Lecce, Italy COMMITTEE: Turbomachinery: Axial Flow Turbine Aerodynamics • Paper Session Room B3-M4 • FB-34-7 lPT lOW REynOldS nuMBER And TRAnSITIOn Session Chair: Thomas Praisner, Pratt and Whitney, East Hartford, CT, USA • Session Co-Chair: John Clark, Air Force Research Laboratory, Wright-Patterson AFB, OH, USA Surface Thin Film gauge Measurements in a Two-Stage low Pressure Turbine at low Reynolds number GT2012-68906 Matthias Kürner, Institute of Aircraft Propulsion System, Universität Stuttgart, Stuttgart, Germany, Martin Rose, Stephan Staudacher, Stuttgart University, Stuttgart, Germany, Jochen Gier, Bastian Patzer, Andreas Fiala, MTU Aero Engines GmbH, München, Germany Boundary layer Control on a low Pressure Turbine Blade by Means of Pulsed Blowing GT2012-69029 Marion Mack, Universität der Bundeswehr München, München, Germany, Andreas Fiala, Yavuz Guendogdu, MTU Aero Engines GmbH, München, Germany, Reinhard Niehuis, University of the German Federal Armed Forces Munich, Neubiberg, Germany The Effect of Acoustic Excitation on Boundary layer Separation of a Highly loaded lPT Blade GT2012-69618 Chiara Bernardini, Stuart Benton, Jeffrey Bons, The Ohio State University, Columbus, OH, USA Axial loss development in low Pressure Turbine Cascades GT2012-69726 Bastian Muth, Reinhard Niehuis, University of the German Federal Armed Forces Munich, Neubiberg, Germany On the Assessment of Turbine Efficiency from Experimental data for low Pressure Turbines at low Reynolds numbers GT2012-69435 Carsten Schneider, Martin G. Rose, Stephan Staudacher, Institute of Aircraft Propulsion System, Universität Stuttgart, Stuttgart, Germany, Adam Heisler, Franz Lippl, Irene Raab, MTU Aero Engines GmbH, Munich, Germany
Look for this Symbol R for Gas Turbine User Related Sessions ASME TURBO EXPO 2012 FINAL PROGRAM 124 FRIDAY JUNE 15: 10:15 a.m. - 12:45 p.m. 10:15 10:45 11:15 11:45 12:15 COMMITTEE: Turbomachinery: design Methods & CFd Modeling for Turbomachinery • Paper Session Room B5-M4 • FB-35-10 OPTIMIzATIOn 2 - TuRBInE APPlICATIOnS Session Chair: S. g. gegg, Rolls Royce Corporation, Indianapolis, IN, USA Three-dimensional design Optimisation of Multistage Axial Flow Turbines using an RSM Based Approach GT2012-68040 Carlo Cravero, Paolo Macelloni, Università di Genova, Genova, Italy, Giuseppe Briasco, Consorzio Sire, Savona, Italy Aerodynamic Optimisation of High Pressure Turbines for lean-Burn Combustion System GT2012-69228 Shahrokh Shahpar, Rolls-Royce, Derby, UK, Stefano Caloni, Rolls Royce, Derby, Derbyshire, UK nozzle guide Vane Cooling System Optimization GT2012-69600 Julian Girardeau, Frederic Pardo, Turbomeca Safran Group, Bordes, France, Jerome Pailhes, Jean Pierre Nadeau, Institut d’Ingénierie et de Mécanique de Bordeaux (I2M), Talence, France Three-dimensional Pressure Controlled Vortex design of a Turbine Stage GT2012-69140 Qingfeng Deng, Qun Zheng, Guoqiang Yue, Hai Zhang, Mingcong Luo, Harbin Engineering University, Harbin, Heilongjiang, China Multidisciplinary Optimization of a Turbocharger Radial Turbine GT2012-68403 Lasse Mueller, Turbomachinery and Propulsion Department, Von Karman Institute for Fluid Dynamics, Rhode-St- Genèse, Belgium, Zuheyr Alsalihi, Tom Verstraete, Von Karman Institute for Fluid Dynamics, Sint-Genesius-Rode, Belgium COMMITTEE: Turbomachinery: Radial Turbomachinery Aerodynamics • Paper Session Room BV2/3 • FB-38-2 CEnTRIFugAl COMPRESSORS II (dESIgn And FlOW AnAlySIS) Session Chair: Hideaki Tamaki, IHI Corporation, Yokohama, Japan • Session Co-Chair: Andre Hildebrandt, MAN Diesel & Turbo SE, Oberhausen, Germany Experimental Study of the Effect of the Tip Clearance to the diffuser Flow Field and Stage Performance of a Centrifugal Compressor GT2012-68445 Ahti Jaatinen, Teemu Turunen-Saaresti, Aki Grönman, Pekka Röyttä, Jari Backman, Lappeenranta University of Technology, Lappeenranta, Finland The Potential of Rotor and Stator Clocking in a 2.5-Stage low-Speed Axial Compressor GT2012-68353 Jörn Städing, Jens Friedrichs, University of Braunschweig, Institute of Jet Propulsion and Turbomachinery, Braunschweig, Germany, Thorsten Waitz, Christoph Dobriloff, Berlin Institute of Technology, Berlin, Germany, Bernd Becker, Volker Gümmer, Rolls-Royce Deutschland Ltd & Co KG, Dahlewitz, Germany Experimental and numerical Investigation of the Flow Field in the Radial Inlet of a Centrifugal Compressor GT2012-69353 Fenghui Han, Datong Qi, Li Wang, Yijun Mao, Xi’an Jiaotong University, Xi’an, Shaanxi, China, Jiajian Tan, Shenyang Blower Works Group Co., Ltd, Shenyang, Liaoning, China Investigation of Separating and utilizing the Influences of up- And downstream Blade Rows GT2012-68371 Ben Zhao, Ce Yang, Du Li, Beijing Institute of Technology, Beijing, China, Liangjun Hu, Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing, China, Mi Zhou, Bohai Shipbuilding Vocational College, Huludao, China Influence of the Swirling Flow in the Side Cavities of a High-Pressure Centrifugal Compressor on the Characteristics of Excited Acoustic Modes GT2012-68380 N. Petry, Siemens AG, Duisburg, Germany, Friedrich Benra, University of Duisburg- Essen, Duisburg, Germany, S. König, Siemens AG, Duisburg, Germany numerical Study on the Effects of Casing Treatment on unsteadiness of Tip leakage Flow in an Axial Compressor GT2012-68444 Yoojun Hwang, Shin-Hyoung Kang, Seoul National University, Seoul, Korea (Republic) Impeller-diffuser Spacing in Centrifugal Compressors GT2012-69151 Chris Robinson, Michael Casey, PCA Engineers Limited, Lincoln, UK, Brad Hutchinson, ANSYS Canada Ltd, Waterloo, ON, Canada, Robin Steed, ANSYS Canada Ltd., Waterloo, ON, Canada Shock Induced Vortices in Transonic Compressors: Aerodynamic Effects and design Correlations GT2012-69004 Henry Knobbe, DLR German Aerospace Centre, Cologne, Germany, Eberhard Nicke, DLR, Cologne, Germany design Optimization and Experimental Verification of Centrifugal Compressors with Curvilinear Element Blades GT2012-69162 Kazuyuki Sugimura, Hitachi, Ltd., Hitachinaka, Ibaraki, Japan, Hiromi Kobayashi, Hideo Nishida, Hitachi Plant Technologies,Ltd., Ibaraki, Japan COMMITTEE: Turbomachinery: unsteady Flows in Turbomachinery • Paper Session Room B5-M2 • FB-40-7 unSTEAdy COMPRESSOR InTERACTIOnS Session Chair: nicole Key Influence of Inlet guide Vane Wakes on the Passage Flow in a Transonic Axial Compressor GT2012-69485 Sebastian Leichtfuss, Christoph Biela, TU Darmstadt, Darmstadt, Germany, Heinz- Peter Schiffer, Technische Universität Darmstadt, Darmstadt, Hessen, Germany, Frank Heinichen, Rolls-Royce Deutschland, Dahlewitz, Germany COMMITTEE: Wind Energy • Paper Session Room B3-M2 • FB-41-11 nOVEl COnCEPTS Session Chair: Ryo Amano, University of Wisconsin-Milwaukee, Glendale, WI, USA • Session Co-Chair: Horacio Perez-Blanco, Penn State, Univesity Park, PA, USA novel Vertical-Axis Wind Turbine with Articulated Blading GT2012-68969 Herbert Jericha, Emil Goettlich, Thorsten Selic, Wolfgang Sanz, Graz University of Technology, Graz, Austria novel Wind Turbine for Catabitic Winds GT2012-69263 Herbert Jericha, Emil Goettlich, Wolfgang Sanz, Graz University of Technology, Graz, Austria development of an Experimental Setup for double Rotors Hawt Investigation GT2012-70032 Ali-Khedher Al-Abadi, Oezguer Ertunc, Philipp Epple, Wolfram Koerbel, Antonio Delgado, University of Erlangen, Erlangen, Germany
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Dear Turbo Expo 2012 Participants:
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6 Networking Events grand Opening M
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8 Participating Organizations Turbo
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12 Facility Tours Take advantage of
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16 Exhibit Hall Floor Plan Subject
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PLEASE REFER TO ONLINE EXHIBITOR DI
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your career... your thirst for know
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30 Technical Conference The Technic
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32 Joint Sessions Coal, Biomass & A
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Look for this Symbol R for Gas Turb
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