
- COPYRIGHT 2004 by ASME Proceedings of ASME TURBO EXPO 2004
- Temperature and Heat Transfer Measurements Cengiz Camci
- TIP DESENSITIZATION OF AN AXIAL TURBINE ROTOR
- 4. ANKARA INTERNATIONAL AEROSPACE CONFERENCE AIAC-2007-004 10-12 September, 2007 -METU, Ankara
- International Journal of Rotating Machinery, 8(2): 109123, 2002 Copyright # 2002 Taylor & Francis
- ELLIPTICAL PIN FINS AS AN ALTERNATIVE TO CIRCULAR PIN FINS FOR GAS TURBINE BLADE COOLING APPLICATIONS
- 32 Progress in Computational Fluid Dynamics, Vol. 10, No. 1, 2010 Copyright 2010 Inderscience Enterprises Ltd.
- ELLIPTICAL PIN FINS AS AN ALTERNATIVE TO CIRCULAR PIN FINS FOR GAS TURBINE BLADE COOLING APPLICATIONS
- Int. Symp. on Heat Transfer in Gas Turbine Systems 9 14 August, 2009, Antalya, Turkey
- 1 COPYRIGHT 2008 by ASME Proceedings of GT2008
- Progress in Computational Fluid Dynamics, Vol. 00, Nos. 0/0, 200x Copyright 2011 Inderscience Enterprises Ltd.
- Proceedings of ASME Turbo Expo Turbine Technical Conference June 6-10, 2011, Vancouver, Canada
- Proceedings of ASME Turbo Expo Turbine Technical Conference June 6-10, 2011, Vancouver, Canada
- 1 Copyright 2011 by ASME Proceedings of ASME Turbo Expo Turbine Technical Conference
- Heat Transfer Research, 2010, Vol. 41, No. 6 Turbine Aero-Heat Transfer Studies
- Influence of Tip Clearance and Inlet Flow Distortion on Ducted Fan Performance in VTOL UAVs Graduate Research Assistant
- Double Ducted Fan (DDF) as a Novel Ducted Fan Inlet Lip Separation Control Device
- Progress in Computational Fluid Dynamics, Vol. , Nos. , 2008 1 Copyright 2008 Inderscience Enterprises Ltd.
- COPYRIGHT 2006 by ASME Proceedings of ASME TURBO EXPO 2007
- ISROMAC-11 Proceedings of the International Symposium on Transport Phenomena and Dynamics of Rotating Machinery,
- UZOL & CAMCI1 ENDWALL HEAT TRANSFER, TOTAL PRESSURE LOSS AND WAKE FLOW FIELD
- COPYRIGHT ! 2004 by ASME Proceedings of IMECE 2004
- COPYRIGHT 2004 by ASME Proceedings of ASME TURBO EXPO 2004
- A TURBINE RESEARCH FACILITY TO STUDY TIP DESENSITIZATION INCLUDING COOLING FLOWS
- TIP LEAKAGE FLOW SIMULATION IN AFTRF BLADE PASSAGES
- TIP DESENSITIZATION OF AN AXIAL TURBINE ROTOR
- INJECTION FROM A TIP TRENCH AS A TURBINE TIP DESENSITIZATION METHOD
- Experimental and Computational Visualization and Frequency Measurements of the Jet Oscillation inside a
- International Journal of Rotating Machinery, 8(2): 125140, 2002 Copyright # 2002 Taylor & Francis
- Secondary ow and forced convection heat transfer near endwall boundary layer fences in a 90 turning duct
- PROOF COPY 003104JTM Christopher McLean1
- DEVELOPMENT OF TIP CLEARANCE FLOW DOWNSTREAM OF A ROTOR BLADE WITH COOLANT INJECTION FROM A TIP TRENCH
- Forced Convection Heat Transfer Enhancement Using a Self-oscillating Impinging Planar Jet
- COLOR RECOGNITION FOR TEMPERATURE MEASUREMENTS ON LIQUID CRYSTAL COATED
- Chapter III LIQUID CRYSTAL BASED TEMPERATURE AND HEAT
- LIQUID CRYSTAL BASED TEMPERATURE AND TRANSIENT HEAT TRANSFER MEASUREMENTS ON HIGHLY CURVED SURFACES
- STEADY STATE LIQUID CRYSTAL THERMOGRAPHY AND HEAT TRANSFER MEASUREMENTS ON
- LIQUID CRYSTAL THERMOGRAPHY ON THE FLUID SOLID INTERFACE OF ROTATING SYSTEMS
- FINITE ELEMENT METHOD IN FLUID MECHANICS & HEAT TRANSFER
- DESIGN OF SMALL SCALE GAS TURBINE SYSTEMS FOR UNMANNED-AERIAL VEHICLES
- COPYRIGHT 2005 by ASME Proceedings of GT2005
- Recent Patents on Mechanical Engineering 2010, 3, 000-000 1 1874-477X/10 $100.00+.00 2010 Bentham Science Publishers Ltd.
- ISROMAC-11 Proceedings of the International Symposium on Transport Phenomena and Dynamics of Rotating Machinery,
- Graduate Research Assistant e-mail: aua162@psu.edu
- A new concept for enhanced turbulent transport of heat in internal coolant passages of gas turbine blades is introduced. The new
- INTRODUCTION TO LIQUID CRYSTAL THERMOGRAPHY AND A BRIEF REVIEW OF PAST
- PROOF COPY [HT-10-1203] 025106JHR [HT-10-1203]025106JHR
- College of Engineering ACADEMIC INTEGRITY COMMITTEE
- PRESSURE SENSITIVE PAINT FOR ANALYSIS OF FILM-COOLING EFFECTS ON A GAS
- Graduate Research Assistant Professor of Aerospace Engineering
- INJECTION FROM A TIP TRENCH AS A TURBINE TIP DESENSITIZATION METHOD
- DOUBLE-DUCTED FAN CROSS-RELATED APPLICATIONS
- American Institute of Aeronautics and Astronautics 47th AIAA Aerospace Sciences Meeting and Exhibit AIAA 2009-332
- COPYRIGHT 2003 by ASME AERODYNAMICS OF TIP LEAKAGE FLOWS
- PROOF COPY 004104JTM Christopher McLean1
- EXAMPLES OF ACADEMIC INTEGRITY VIOLATIONS Office of Judicial Affairs, Penn State University
- Vol. , No. , 200x 1 Copyright 200x Inderscience Enterprises Ltd.
- DOUBLE DUCTED FAN (DDF) Cengiz Camci and Ali Akturk
- SIMULATION OF TIP LEAKAGE FLOW AROUND PARTIAL SQUEALER RIMS IN AXIAL TURBINES
- Axial Flow Fan Tip Leakage Flow Control Using Tip Platform Extensions
- Convective Heat Transfer and Reference Free-stream Temperature Determination near the Casing of an Axial Flow
- COPYRIGHT 2008 by ASME1 Proceedings of GT2008
- A COMPUTATIONAL AND EXPERIMENTAL ANALYSIS OF A DUCTED FAN USED IN VTOL UAV SYSTEMS
- Vol. , No. , 200x 1 Copyright 200x Inderscience Enterprises Ltd.
- COPYRIGHT 2003 by ASME IGTI/ASME TURBO EXPO 2003
- ISROMAC-11 Proceedings of the International Symposium on Transport Phenomena and Dynamics of Rotating Machinery,
- COPYRIGHT 2006 by ASME Proceedings of ASME TURBO EXPO 2006
- ISROMAC-11 Proceedings of the International Symposium on Transport Phenomena and Dynamics of Rotating Machinery,
- A COURSE ANNOUNCEMENT FOR SPRING 2002