FINAL PROGRAM - Events

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Look for this symbol ✲ for Gas Turbine user related sessions. FINAL PROGRAM TURBO EXPO 2010 • 46 MONDAY, JUNE 14: 2:30 p.m. – 5:30 p.m. 2:30 3:00 3:30 4:00 4:30 5:00 COMMITTEE: Structures & Dynamics: Non-Deterministic Methods & Applications • Paper Session Room: Boisdale 2 • SECC • MB-21-1 PROBABILISTIC FATIGUE AND FRACTURE Session Chair: Michael Gorelik, Honeywell Aerospace, Phoenix, AZ, USA Session Co-Chair: Phillip Gravett, Siemens Energy Inc., Orlando, FL, USA, Swami Swaminathan, TurboMet International, San Antonio, TX, USA Toward Developing a Probabilistic Methodology for Predicting High-Cycle Fretting Fatigue in Aero-engines GT2010-23007 Kwai S. Chan, Michael P Enright, Harold R. Simmons, Southwest Research Institute, San Antonio, TX, USA, Patrick J. Golden, Air Force Research Laboratory, Dayton, OH, USA, Ramesh Chandra, Alan C. Pentz, NAVAIR, Patuxent River, MD, USA A Probabilistic Framework for Gas Turbine Engine Materials with Multiple Types of Anomalies GT2010-23618 Michael P. Enright, R. Craig McClung, Southwest Research Institute, San Antonio, TX, USA Bayesian Approach for Fatigue Life Prediction from Field Inspection GT2010-23780 Nam Ho Kim, Sriram Pattabhiraman, University of Florida, Gainesville, FL,USA, Lonnie Houck III, Alstom Turbine Technologies, Palm Beach, FL, USA Probabilistic Creep Life Prediction of Turbine Discs GT2010-22169 Ashok Koul, Life Prediction Technologies Inc., Ottawa, ON, Canada Probabilistic Property Prediction Of Aero-Engine Components For Fatigue. GT2010-22708 Hector Basoalto, Jeffery W. Brooks, University of Strathclyde, Glasgow, UK, Paul Tranter, Randeep S. Sahota, QinetiQ, Farnborough, UK COMMITTEE: Structures & Dynamics: Rotordynamics • Paper Session Room: Leven • SECC • MB-22-4 ROTORDYNAMICS I Session Chair: Yong-Bok Lee, Korea Institute of Science and Technology, Seoul, Korea (Republic) Session Co-Chair: Robert Bruckner Non-Linear Maneuver- Acceleration Analysis for Airborne Gas Turbine Engines GT2010-22435 Theodore Brockett, Honeywell International, Inc, Phoenix, AZ, USA Approximation of Critical Speeds for Shafts with Thermal Gradients using a Rotating Heat Rig GT2010-22522 Michael Mixa, Ali P. Gordon, University of Central Florida, Orlando, FL, USA Multiple Smart Material Applications using SMA and MR Fluid Damper for Rotor Vibration Control GT2010-23084 T.S. Aravindhan, MSC Software, Bangalore, India, Kshitij Gupta, Indian Institute of Technology, Delhi, New Delhi, Delhi, India Study on Rubbing Failure between Fan Vanes and Spacer Ring of a Turbo-Fan Engine GT2010-23152 Zhang Dayi, Chen Meng, Hong Jie, Beijing University of Aero. and Astro., Beijing, China, Dou Miansheng, BUAA & AVIC Harbin Dongan Engine (Group) Corporation LTD., Harbin, China Improving the Design of a Compressor Casing With the Help of Finite Element Analysis to Ensure the Rotor Dynamic Stability of High Pressure Centrifugal Compressor Equipped With a Hole Pattern Seal GT2010-22185 Yves Bidaut, Urs Baumann, MAN TURBO AG Schweiz, Zürich, CH, Switzerland Lateral Rotordynamic Analysis Of A Large Alternator/Flywheel/Motor Train GT2010-23585 Jawad Chaudhry, Timothy Dimond, Amir Younan, Paul Allaire, University of Virginia, Charlottesville, VA, USA
For a complete listing of Joint Sessions please see page 34 FINAL PROGRAM TURBO EXPO 2010 • 47 MONDAY, JUNE 14: 2:30 p.m. – 5:30 p.m. 2:30 3:00 3:30 4:00 4:30 5:00 COMMITTEE: Structures & Dynamics: Structural Mechanics & Vibration • Paper Session Room: Morar/Ness • SECC • MB-23-1 MISTUNING OF BLADED DISKS Session Chair: Harald Schoenenborn, MTU Aero Engines GmbH, Munich, Germany Session Co-Chair: Holger Hennings, DLR - German Aerospace Center, Goettingen, Germany Reduced Order Model of a Multistage Bladed Rotor with Geometric Mistuning via Modal Analyses of Finite Element Sectors GT2010-22725 Yasharth Bhartiya, Alok Sinha, The Pennsylvania State University, University Park, PA, USA Forced Response Analysis of Mistuned Steam Turbine Bladings GT2010-23782 Christian Siewert, heinrich stueer, Siemens AG - Energy Sector, Muelheim an der Ruhr, Germany Quantitative Validation of the Asymptotic Mistuning Model (AMM) Using a High Fidelity Bladed Disk Model GT2010-22498 Oualid Khemiri, Carlos Martel, Polytechnic University of Madrid, Madrid, Madrid, Spain, Roque Corral, Industria de Turbopropulsores S.A., San Fernando de Henares, Madrid, Spain Non-Linear Forced Response Analysis of Mistuned Bladed Disk Assemblies GT2010-22128 M. Ersin Yümer, Defense Industries Research and Development Institute, Tübitak-Sage, Ankara,Turkey, Ender Cigeroglu, H. Nevzat Özgüven, Mechanical Engineering Department, Middle East Technical University, Ankara, Turkey Reduction of forced response levels for bladed discs by mistuning: overview of the phenomenon GT2010-23299 Evgeny Petrov, Imperial College London, London, London, UK Mistuning identification for integrally bladed disks based on the SNM technique GT2010-22105 Shuai Wang, Jianyao Yao, Jianjun Wang, Beijing University of Aeronautics and Astronautics, Beijing, China COMMITTEE: Turbomachinery: Axial Flow Fan & Compressor Aerodynamics • Paper Session Room: Castle 1 • Crowne Plaza • MB-26-5 FLOW CONTROL Session Chair: Alessandro Corsini, Dipartimento di Meccanica e Aeronautica, ‘Sapienza’ Università di Roma, Roma, Italy Session Co-Chair: Stefano Bianchi, Sapienza University of Rome, Rome, Italy Study of Flow Control Using a Slotted Blade for a Compressor Airfoil at Low Reynolds Numbers GT2010-22660 Min Zhou, Junqiang Zhu, Xingen Lu,Institute of Engineering Thermophysics, Chinese Academy of Science, Beijing, China, Zhihui Ge, Kexue Yan, Rong Huang, Beijing Aeronautical Technology Research Center, Beijing,China Control of Tip-Clearance Flow in a Low Speed Axial Compressor Rotor with Plasma Actuation GT2010-22345 Giridhar Jothiprasad,, Robert C Murray, Katherine Essenhigh, Grover A Bennett, Seyed G Saddoughi, GE Global Research, Niskayuna, NY, USA, Aspi Wadia, GE Aviation, Cincinnati, OH, USA, Andy Breeze-Stringfellow, GE Global Research, Cincinnati, OH, USA Unsteady RANS simulations of a highly loaded low aspect ratio compressor stator cascade with active flow control GT2010-22516 Christoph Gmelin, Mathias Steger, Berlin University of Technology, Berlin,Germany, Andre Huppertz, Marius Swoboda, Rolls-Royce Deutschland, Blankenfelde- Mahlow, Germany, Prof. Frank Thiele, Technische Universität Berlin, Berlin, Germany On The Efficiency Of Secondary Flow Suction In A Compressor Cascade GT2010-22336 Karsten Liesner, Robert K.J. Meyer,German Aerospace Center (DLR) e.V., Berlin, Germany Matthias Lemke, Prof. Frank Thiele, Technische Universität Berlin, Berlin, Germany, Christoph Gmelin, Berlin University of Technology, Berlin, Germany Experimental Investigation of Endwall and Suction Side Blowing in a Highly Loaded Stator Cascade GT2010-22578 Dr.-Ing. Daniel Nerger, TU Braunschweig, Braunschweig, Germany, PD Dr.-Ing. Horst Saathoff, Prof. Dr.-Ing. Rolf Radespiel, Institut für Strömungsmechanik, Technische Universität Braunschweig, Braunschweig, Germany, Dr.-Ing. Volker Gümmer, Dr.-Ing. Carsten Clemen, OE-1 Compressors and Fans, Rolls-Royce Deutschland Ltd. & Co. KG, Blankenfelde- Mahlow, Germany Numerical Investigations of the Efficiency of Circulation Control in a Compressor Stator GT2010-22721 Arne Vorreiter, Institute of Turbomachinery and Fluid Dynamics / Leibniz Universitaet Hannover, Hannover, Germany, S. Fischer, R. Radespiel, Institute of Fluid Mechanics, Technische Universitaet Braunschweig, Braunschweig, Germany, Horst Saathoff, Siemens AG - Energy Sector, Mülheim an der Ruhr, Germany, Joerg Seume, Leibniz Universitaet Hannover, Hannover, Germany
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REGISTRATION HOURS Sunday, June 13
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HEAT TRANSFER Richard B. Rivir AFRL
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ASME International Gas Turbine Inst
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