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Look for this symbol ✲ for Gas Turbine user related sessions. FINAL PROGRAM TURBO EXPO 2010 • 112 THURSDAY, JUNE 17: 2:30 p.m. – 5:30 p.m. 2:30 3:00 3:30 4:00 4:30 5:00 COMMITTEE: Heat Transfer: General Interest • Paper Session Room: Gala 1 • SECC • ThC-9-8 ROTATIONAL EFFECTS ON INTERNAL COOLING Session Chair: Nirm Nirmalan, GE Global Research Center, Niskayuna, NY, USA Session Co-Chair: Gregory Laskowski, General Electric Global Research, Niskayuna, NY, USA Heat Transfer In Trailing Edge Wedge-Shaped Pin-Fin Channels With Slot Ejection Under High Rotation Numbers GT2010-22832 Akhilesh P. Rallabandi, Je- Chin Han, Texas A&M University, College Station, TX,USA, Yah-Hsien Liu, National Chiao Tung University, Hsinchu, Taiwan Numerical Predictions of the Effect of Rotation on Fluid Flow and Heat Transfer in an Engine- Similar Two-Pass Internal Cooling Channel with Smooth and Ribbed Walls GT2010-22870 Marco Schüler, Horst-Michael Dreher, Sven Olaf Neumann, Universität Stuttgart, Institut für Thermodynamik der Luft- und Raumfahrt (ITLR), Stuttgart, Germany, Martin Elfert, German Aerospace Centre (DLR), Institute of Propulsion Technology, Cologne, Germany, , Bernhard Weigand, Institute of Aerospace Thermodynamics (ITLR), Universität Stuttgart, Stuttgart, Germany PIV-Measurement of Secondary Flow in a Rotating Two-Pass Cooling System with an Improved Sequencer Technique GT2010-23510 Martin Elfert, German Aerospace Centre (DLR), Institute of Propulsion Technology, Cologne, Germany, Michael Schroll, Wolfgang Foerster, German Aerospace Center (DLR), Koeln, Germany Influence Of Channel Orientation On Heat Transfer In A Two-Pass Smooth And Ribbed Rectangular Channel (AR=2:1) Under Large Rotation Numbers GT2010-22190 Michael Huh, The University of Texas at Tyler, Tyler, TX, USA, Jiang Lei, Je-Chin Han, Texas A&M University, College Station, TX, USA Investigation of Coriolis Forces Effect of Flow Structure and Heat Transfer Distribution in a Rotating Dimpled Channel GT2010-22657 Mohammad Elyyan, ANSYS Inc, Austin, TX, USA, Danesh K. Tafti, Virginia Tech, Blacksburg, VA, USA Heat Transfer in a Rotating Rectangular Channel With Two Opposite Walls Roughened with Spherical Protrusions at High Rotation Numbers GT2010-22609 Shyy Woei Chang, National Kaohsiung Marine University, Kaohsiung, Taiwan, T.-M. Liou, Department of Power Mechanical Engineering, Hsinchu, Taiwan, China, W. G. Chen, National Tsing Hua Marine University, Tsinghua, China COMMITTEE: Heat Transfer: Film Cooling • Paper Session Room: Alsh 2 • SECC • ThC-10-5 ANALYTICAL MODELING OF FILM COOLING Session Chair: Savas Yavuzkurt, The Pennsylvania State University, University Park, PA, USA Session Co-Chair: Cengiz Camci, Penn State University, Boalsburg, PA, USA Block-Spectral Approach to Film-Cooling Modelling GT2010-22188 Li He, University of Oxford, Oxford, Oxford, UK A Model for Cylindrical Hole Film Cooling: Part I - A Correlation for Jet-Flow with Application to Film Cooling GT2010-22787 Tilman Auf dem Kampe, Stefan Voelker, Siemens AG, Energy Sector, Mülheim a. d. Ruhr, Germany, Frank N. Zehe, University Stuttgart, Stuttgart, Germany A Model for Cylindrical Hole Film Cooling: Part II - Model Formulation, Implementation and Results GT2010-22788 Tilman Auf dem Kampe, Stefan Voelker, Siemens AG, Energy Sector, Muelheim a. d. Ruhr, Germany A Correlation Approach to Predicting Film Cooled Turbine Vane Heat Transfer GT2010-23597 Bob Boyle, NNR, Cleveland, OH, USA, Ali Ameri, The Ohio State University, Cleveland, OH, USA Aerothermodynamics Of A High-Pressure Turbine Blade With Very High Loading And Vortex Generators GT2010-23543 Reinaldo Araujo Gomes, University of the Federal Armed Forces Munich, Munich, Germany, Reinhard Niehuis, Institute of Jet Propulsion, University of the Federal Armed Forces Munich, Neubiberg, Bavaria, Germany
For a complete listing of Joint Sessions please see page 34 FINAL PROGRAM TURBO EXPO 2010 • 113 THURSDAY, JUNE 17: 2:30 p.m. – 5:30 p.m. 2:30 3:00 3:30 4:00 4:30 5:00 COMMITTEE: Heat Transfer: Internal Air and Seals (with Turbomachinery Committee) • Paper Session Room: Alsh 1 • SECC • ThC-11-7 SECONDARY FLOW SYSTEM DESIGN Session Chair: Peter R N Childs, Imperial College London, London, UK Session Co-Chair: Jeff Dixon, Rolls-Royce plc, Derby, Derbyshire, UK A Probabilistic Secondary Flow System Design Process for Gas Turbine Engines GT2010-22071 Alex MirzaMoghadam, Douglas Ramerth, Honeywell International, Phoenix, AZ, USA, Ashish Kiratsingh, Gaurav Banda, Honeywell Technical Solutions Lab, Bangalore, 10, India Impacts of Engine Secondary Air System Uncertainties On Gas Turbine Compressor Heat Transfer GT2010-23392 Sohail Alizadeh, Atkins (Fluid Mechanics), Epsom, UK, Naveen Prasad Gopinathrao, Atkins, Epsom, UK 1D Tool for Stator-Rotor Cavities Integrated into a Fluid Network Model of Heavy-Duty Gas Turbine Secondary Air System GT2010-22203 Luca Bozzi, Marco Mantero, Federico Bonzani, Alessandro Vinci, Ansaldo Energia, Genova, Italy, Luca Innocenti, Mirko Micio, Università degli Studi di Firenze - Dipartimento di Energetica “Sergio Stecco”, Firenze, Firenze, Italy, An Efficient Procedure for the Analysis of Heavy Duty Gas Turbine Secondary Flows in Different Operating Conditions GT2010-22935 Luca Bozzi, Federico Bonzani, Ansaldo Energia, Genova, Italy, Carlo Carcasci, Università degli Studi di Firenze - Dipartimento di Energetica, Firenze, Italy, Matteo Cerutti, CFD Engineering S.r.l., Firenze, Italy, Transient Thermodynamic, Thermal And Structure Analysis Of A Steam Turbine During Its Start-Up GT2010-22813 Rzadkowski Romuald, Lampart Piotr, Kwapisz Leszek, Szymaniak Mariusz, Drewczynski Marcin, Polish Academy of Sciences, Institute of Fluid-Flow Machinery, Gdansk, Poland COMMITTEE: Heat Transfer: Transition (with Turbomachinery Committee) • Paper Session Room: Carron 2 • SECC • ThC-12-2 TRANSITION SESSION Session Chair: Phillip Ligrani, Siemens Energy Inc., Orlando, FL, USA Session Co-Chair: Ting Wang, University of New Orleans, New Orleans, LA, USA Calculation Of Steady And Periodic Unsteady Blade Surface Heat Transfer In Separated Transitional Flow GT2010-23275 Roberto Pacciani, Filippo Rubechini, Andrea Arnone, University of Florence, Florence, Italy, Ewald Lutum, MTU Aero Engines GmbH, Munich, Germany Modeling separation induced transition using a non-linear three equation turbulence model and a Reynolds stress turbulence model. GT2010-23331 Zinon Vlahostergios, Kyros Yakinthos, Lab. of Fluid Mechanics and Turbomachinery, Dept. of Mechanical Engineering, Aristotle University, Thessaloniki, Greece Experimental Heat Transfer Investigation In A Multisplitter LP Vane Architecture GT2010-22694 Victor Pinilla, Juan Pedro Solano, Dr. Guillermo Paniagua, Sergio Lavagnoli, Tolga Yasa, von Karman Institute, Rhode St. Genese, Belgium Sensitivity of Numerical Simulations of Low- Reynolds Fow over the T106 Turbine Blade GT2010-22903 Xavier de Saint Victor, ONERA, Toulouse, France (Metro)
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FINAL PROGRAM Presented by ASME Int
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Executive Conference Chair Dr. Grah
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Honorary Lectures Industrial Gas Tu
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Women Working in the Gas Turbine Ar
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PHOTO COURTESy OF THE UnITED STATES
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