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TURBOMACHINERY AERO-HEAT TRANSFER LABORATORY

TURBOMACHINERY AERO-HEAT TRANSFER LABORATORY. THE PENNSYLVANIA STATE UNIVERSITY Dr. Cengiz Camci Professor of Aerospace Engineering 223 Hammond Building http://www.personal.psu.edu/cxc11/AFTRF Presented to P&W visitors on 7/9/2009. TURBOMACHINERY AERO-HEAT TRANSFER LABORATORY

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TURBOMACHINERY AERO-HEAT TRANSFER LABORATORY

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  1. TURBOMACHINERY AERO-HEAT TRANSFER LABORATORY THE PENNSYLVANIA STATE UNIVERSITY Dr. Cengiz Camci Professor of Aerospace Engineering 223 Hammond Building http://www.personal.psu.edu/cxc11/AFTRF Presented to P&W visitors on 7/9/2009

  2. TURBOMACHINERY AERO-HEAT TRANSFER LABORATORY Dept.of Aerospace Engineering RESEARCH & FACILITIES COURSES & SPONSORS Prepared by : Dr. Cengiz Camci Professor of Aerospace Engineering 223 Hammond Building cxc11@psu.edu http://www.personal.psu.edu/cxc11bb Presented to P&W visitors on 7/9/2009

  3. Non-intrusive turbine aero-heat transfer measurements • LDA, PIV, thermographic liquid crystals • pressure sensitive paints and infrared thermography • Numerical prediction of turbomachinery flow and heat transfer in a high performance computer cluster FLUID DYNAMICS & HEAT TRANSFER STUDIES APPLIED TO TURBOMACHINERY SYSTEMS • Aero-heat transfer studies of turbine casing treatments • Turbine blade tip aero-heat transfer studies including novel squealer tips and tip leakage de-sensitization devices • Turbine disk cavity flows and intra-stage leakage aerodynamics • Turbine blade tip injection studies • Secondary flow minimization • (NGV and blade) Endwall contouring including non-axisymmetric contouring

  4. TURBOMACHINERY RELATED TEACHING EFFORTS • Theory and Design of Turbomachinery AERSP 507 • Aero-thermo-mechanical Design of Small Gas Turbines for UAV Applications AERSP 597-K • Propulsion System Design and Analysis for Unmanned Air Vehicles AERSP 597-E • Finite Element Method in Fluid Mechanics and Heat Transfer AERSP 560 • Foundations of Fluid Mechanics AERSP 508 • Aerospace Propulsion AERSP 410 • Turbulent Flow AERSP 412

  5. MAJOR TURBOMACHINERY RESEARCH FACILITIES • HEAT TRANSFER WIND TUNNEL • LOW SPEED LINEAR CASCADE • HIGH SPEED FLOW facility 600 HP blower, dP=225 ” of H2O Mach 0.8 flow at cascade exit • A 36 INCH DIAM. TURBINE RESEARCH FACILITY (a large scale, rotating, cold flow turbine rig) • AXIAL FLOW FAN/DUCTED FAN RESEARCH FACILITY • PLANAR AND STEREOSCOPIC PIV SYSTEMS • VARIOUS PROBE CALIBRATION SYSTEMS • LIQUID CRYSTAL AND PSP CALIBRATION SYSTEMS

  6. RECENT EMPHASIS AREAS ARE: Aero-heat transfer studies of turbine casing treatments General turbine heat transfer studies (gas side and coolant side) Turbine blade tip aero-heat transfer studies including novel squealer tips and tip leakage de-sensitization devices Turbine disk cavity flows and intra-stage leakage aerodynamics Turbine blade tip injection studies Secondary flow minimization (NGV and blade) Endwall contouring including non-axisymmetric contouring Non-intrusive turbine aero-heat transfer measurements including, LDA, PIV, thermographic liquid crystals, pressure sensitive paints and infrared thermography Numerical prediction of turbomachinery flow and heat transfer in a high performance computer

  7. Past Sponsors : • Von Karman Institute for Fluid Dynamics, Belgium NASA • Ecole Centrale Lyon, France • Istanbul Technical University • International Center for Heat and Mass Transfer ICHMT _______________________________________________ • Lewis/Glenn Research Center • National Science Foundation (CTS) • DOE/AGTSR/SCIES • DOD/Army Research Office • Pratt& Whitney Aircraft Engines • GE GRC/PS • Solar Turbines/Caterpillar • Trane Corporation • Siemens Energy • Sikorsky Aircraft Company (SAC)/UTRC • Center for Rotorcraft Innovation CRI

  8. TURBOMACHINERY AERO-HEAT TRANSFER LABORATORYPennsylvania State UniversityDept.of Aerospace Engineering For further details contact to: Dr.Cengiz Camci Dept. of Aerospace Engineering 223 Hammond Building University Park PA 16802 cxc11@psu.edu http://www.personal.psu.edu/cxc11

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