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

RESEARCH & FACILITIES COURSES & SPONSORS 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

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 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

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

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

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

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

Dept. of Aerospace Engineering TURBOMACHINERY AERO-HEAT TRANSFER LABORATORY Pennsylvania State University Dept.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