AFTRF capabilities Cengiz Camci

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TURBOMACHINERY AERO-HEAT TRANSFER LABORATORY
THE PENNSYLVANIA STATE UNIVERSITY Dr. Cengiz
Camci Professor of Aerospace Engineering 223
Hammond Building http//www.personal.psu.edu/cxc1
1/AFTRF Presented to PW visitors on 7/9/2009
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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_at_psu.edu http//www.personal.psu.edu/cxc11bb
Presented to PW visitors on 7/9/2009
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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

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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

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MAJOR TURBOMACHINERY RESEARCH FACILITIES

• HEAT TRANSFER WIND TUNNEL

• LOW SPEED LINEAR CASCADE

• HIGH SPEED FLOW facility 600 HP blower, dP225
  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

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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

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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

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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_at_psu.edu
http//www.personal.psu.edu/cxc11