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Proc. ASME. GT2022, Volume 10B: Turbomachinery — Axial Flow Turbine Aerodynamics; Deposition, Erosion, Fouling, and Icing; Radial Turbomachinery Aerodynamics, V10BT30A006, June 13–17, 2022

Publisher: American Society of Mechanical Engineers

Paper No: GT2022-80607

https://doi.org/10.1115/GT2022-80607

View Paper titled, A Framework for Estimating Effects of Combustor Turbulence on Turbine Profile Loss Generation

Topics: Combustion chambers, Turbines, Turbulence, High pressure (Physics), Energy dissipation, Aircraft engines, Boundary layer turbulence, Boundary layers, Gas turbines, Gates (Closures)

Journal Articles

Effects of Surface Waviness on Fan Blade Boundary Layer Transition and Profile Loss—Part I: Methodology and Computational Results

Jinwook Lee, Zoltán S. Spakovszky, Edward M. Greitzer, Mark Drela, Jérôme Talbotec

Publisher: ASME

J. Turbomach. February 2022, 144(2): 021001.

Paper No: TURBO-21-1159

https://doi.org/10.1115/1.4052235

Published Online: September 22, 2021

View Article titled, Effects of Surface Waviness on Fan Blade Boundary Layer Transition and Profile Loss—Part I: Methodology and Computational Results

Topics: Blades, Boundary layers, Flow (Dynamics), Wavelength, Waves, Acoustics

Journal Articles

Effects of Surface Waviness on Fan Blade Boundary Layer Transition and Profile Loss—Part II: Experimental Assessments and Applications

Jinwook Lee, Vaishnavi Ramaswamy, Zoltán S. Spakovszky, Edward M. Greitzer, Mark Drela, Jérôme Talbotec

Publisher: ASME

J. Turbomach. February 2022, 144(2): 021002.

Paper No: TURBO-21-1160

https://doi.org/10.1115/1.4052236

Published Online: September 22, 2021

View Article titled, Effects of Surface Waviness on Fan Blade Boundary Layer Transition and Profile Loss—Part II: Experimental Assessments and Applications

Topics: Blades, Boundary layers, Chords (Trusses), Wavelength, Waves, Thermography, Design, Surface waves (Fluid)

Proceedings Papers

Effects of Surface Waviness on Fan Blade Boundary Layer Transition and Profile Loss — Part I: Methodology and Computational Results

Jinwook Lee, Zoltán S. Spakovszky, Edward M. Greitzer, Mark Drela, Jérôme Talbotec

Proc. ASME. GT2021, Volume 2A: Turbomachinery — Axial Flow Fan and Compressor Aerodynamics, V02AT31A010, June 7–11, 2021

Publisher: American Society of Mechanical Engineers

Paper No: GT2021-58676

https://doi.org/10.1115/GT2021-58676

View Paper titled, Effects of Surface Waviness on Fan Blade Boundary Layer Transition and Profile Loss — Part I: Methodology and Computational Results

Topics: Blades, Boundary layers, Wavelength, Acoustics, Composite materials, Computation, Energy transformation, Flow (Dynamics), Noise (Sound), Surface waves (Fluid)

Proceedings Papers

Effects of Surface Waviness on Fan Blade Boundary Layer Transition and Profile Loss — Part II: Experimental Assessments and Applications

Jinwook Lee, Vaishnavi Ramaswamy, Zoltán S. Spakovszky, Edward M. Greitzer, Mark Drela, Jérôme Talbotec

Proc. ASME. GT2021, Volume 2A: Turbomachinery — Axial Flow Fan and Compressor Aerodynamics, V02AT31A011, June 7–11, 2021

Publisher: American Society of Mechanical Engineers

Paper No: GT2021-58678

https://doi.org/10.1115/GT2021-58678

View Paper titled, Effects of Surface Waviness on Fan Blade Boundary Layer Transition and Profile Loss — Part II: Experimental Assessments and Applications

Topics: Blades, Boundary layers, Wavelength, Surface waves (Fluid), Aircraft, Composite materials, Delays, Resonance, Reynolds number, Thermography

Proceedings Papers

Endwall Blockage in Axial Compressors

S. Arif Khalid, Amrit S. Khalsa, Ian A. Waitz, Choon S. Tan, Edward M. Greitzer, Nicholas A. Cumpsty, John J. Adamczyk, Frank E. Marble

Proc. ASME. GT1998, Volume 1: Turbomachinery, V001T01A047, June 2–5, 1998

Publisher: American Society of Mechanical Engineers

Paper No: 98-GT-188

https://doi.org/10.1115/98-GT-188

View Paper titled, Endwall Blockage in Axial Compressors

Topics: Compressors, Clearances (Engineering), Flow (Dynamics), Design, Blades, Boundary layers, Computer simulation, Pressure, Wind tunnels

Proceedings Papers

Role of Blade Passage Flow Structures in Axial Compressor Rotating Stall Inception

Donald A. Hoying, Choon S. Tan, Huu Duc Vo, Edward M. Greitzer

Proc. ASME. GT1998, Volume 1: Turbomachinery, V001T01A138, June 2–5, 1998

Publisher: American Society of Mechanical Engineers

Paper No: 98-GT-588

https://doi.org/10.1115/98-GT-588

View Paper titled, Role of Blade Passage Flow Structures in Axial Compressor Rotating Stall Inception

Topics: Blades, Compressors, Flow (Dynamics), Stall inception, Clearances (Engineering), Vortices, Compression, Computation, Kinematics, Stability

Proceedings Papers

Effects of Inlet Flow Field Conditions on the Performance of Centrifugal Compressor Diffusers: Part 1 — Discrete-Passage Diffuser

Victor G. Filipenco, Sabri Deniz, J. Mark Johnston, Edward M. Greitzer, Nicholas A. Cumpsty

Proc. ASME. GT1998, Volume 1: Turbomachinery, V001T01A111, June 2–5, 1998

Publisher: American Society of Mechanical Engineers

Paper No: 98-GT-473

https://doi.org/10.1115/98-GT-473

View Paper titled, Effects of Inlet Flow Field Conditions on the Performance of Centrifugal Compressor Diffusers: Part 1 — Discrete-Passage Diffuser

Topics: Compressors, Diffusers, Flow (Dynamics), Pressure, Mach number, Axial flow, Boundary layers, Flow instability, Momentum, Test facilities

Proceedings Papers

Effects of Inlet Flow Field Conditions on the Performance of Centrifugal Compressor Diffusers: Part 2 — Straight-Channel Diffuser

Sabri Deniz, Edward M. Greitzer, Nicholas A. Cumpsty

Proc. ASME. GT1998, Volume 1: Turbomachinery, V001T01A112, June 2–5, 1998

Publisher: American Society of Mechanical Engineers

Paper No: 98-GT-474

https://doi.org/10.1115/98-GT-474

View Paper titled, Effects of Inlet Flow Field Conditions on the Performance of Centrifugal Compressor Diffusers: Part 2 — Straight-Channel Diffuser

Topics: Compressors, Diffusers, Flow (Dynamics), Pressure, Mach number, Axial flow, Momentum, Wedges

Journal Articles

Blade Loading Effects on Axial Turbine Tip Leakage Vortex Dynamics and Loss

Arthur C. Huang, Edward M. Greitzer, Choon S. Tan, Eugene F. Clemens, Steven G. Gegg, Edward R. Turner

Publisher: ASME

J. Turbomach. September 2013, 135(5): 051012.

Paper No: TURBO-12-1092

https://doi.org/10.1115/1.4007832

Published Online: June 26, 2013

View Article titled, Blade Loading Effects on Axial Turbine Tip Leakage Vortex Dynamics and Loss

Topics: Blades, Clearances (Engineering), Flow (Dynamics), Leakage, Pressure, Turbines, Vortices, Leakage flows, Suction

Journal Articles

Some Aerodynamic Problems of Aircraft Engines: Fifty Years After -The 2007 IGTI Scholar Lecture-

Edward M. Greitzer

Publisher: ASME

J. Turbomach. July 2009, 131(3): 031101.

https://doi.org/10.1115/1.2992515

Published Online: April 20, 2009

View Article titled, Some Aerodynamic Problems of Aircraft Engines: Fifty Years After -The 2007 IGTI Scholar Lecture-

Topics: Aircraft, Collaboration, Compressors, Design, Engines, Gas turbines, International Gas Turbine Institute, Surges, Flow (Dynamics), Feedback

Proceedings Papers

Some Aerodynamic Problems of Aircraft Engines: Fifty Years After

Edward M. Greitzer

Proc. ASME. GT2007, Volume 1: Turbo Expo 2007, 991-1007, May 14–17, 2007

Publisher: American Society of Mechanical Engineers

Paper No: GT2007-28364

https://doi.org/10.1115/GT2007-28364

View Paper titled, Some Aerodynamic Problems of Aircraft Engines: Fifty Years After

Topics: Aircraft, Aircraft engines, Collaboration, Engineering disciplines, Gas turbines, Jet engines, Product development, Teams

Proceedings Papers

Criteria for Spike Initiated Rotating Stall

Huu Duc Vo, Choon S. Tan, Edward M. Greitzer

Proc. ASME. GT2005, Volume 6: Turbo Expo 2005, Parts A and B, 155-165, June 6–9, 2005

Publisher: American Society of Mechanical Engineers

Paper No: GT2005-68374

https://doi.org/10.1115/GT2005-68374

View Paper titled, Criteria for Spike Initiated Rotating Stall

Topics: Blades, Clearances (Engineering), Compressors, Computation, Computer simulation, Engineering simulation, Flow (Dynamics), Fluids, Simulation, Stall inception

Journal Articles

Criteria for Spike Initiated Rotating Stall

Huu Duc Vo, Choon S. Tan, Edward M. Greitzer

Publisher: ASME

J. Turbomach. January 2008, 130(1): 011023.

https://doi.org/10.1115/1.2750674

Published Online: January 30, 2008

View Article titled, Criteria for Spike Initiated Rotating Stall

Topics: Blades, Clearances (Engineering), Flow (Dynamics), Stall inception, Rotors, Compressors, Computation

Journal citation

NARROW

Tail-Integrated Boundary Layer Ingesting Propulsion Systems for Turbo-Electric Aircraft

Tail-Integrated Boundary Layer Ingesting Propulsion Systems for Turbo-Electric Aircraft

Basic Research Issues in Aerodynamics, Structural Dynamics, and Control of Turbine Engine High Cycle Fatigue

A Framework for Estimating Effects of Combustor Turbulence on Turbine Profile Loss Generation

A Framework for Estimating Effects of Combustor Turbulence on Turbine Profile Loss Generation

Effects of Surface Waviness on Fan Blade Boundary Layer Transition and Profile Loss—Part I: Methodology and Computational Results

Effects of Surface Waviness on Fan Blade Boundary Layer Transition and Profile Loss—Part II: Experimental Assessments and Applications

Effects of Surface Waviness on Fan Blade Boundary Layer Transition and Profile Loss — Part I: Methodology and Computational Results

Effects of Surface Waviness on Fan Blade Boundary Layer Transition and Profile Loss — Part II: Experimental Assessments and Applications

Endwall Blockage in Axial Compressors

Role of Blade Passage Flow Structures in Axial Compressor Rotating Stall Inception

Effects of Inlet Flow Field Conditions on the Performance of Centrifugal Compressor Diffusers: Part 1 — Discrete-Passage Diffuser

Effects of Inlet Flow Field Conditions on the Performance of Centrifugal Compressor Diffusers: Part 2 — Straight-Channel Diffuser

Blade Loading Effects on Axial Turbine Tip Leakage Vortex Dynamics and Loss

Some Aerodynamic Problems of Aircraft Engines: Fifty Years After -The 2007 IGTI Scholar Lecture-

Some Aerodynamic Problems of Aircraft Engines: Fifty Years After

Criteria for Spike Initiated Rotating Stall

Criteria for Spike Initiated Rotating Stall

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