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Proceedings Papers

A Three-Dimensional Turbine Engine Analysis Compressor Code (TEACC) for Steady-State Inlet Distortion

Proc. ASME. GT1997, Volume 4: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; IGTI Scholar Award, V004T16A005, June 2–5, 1997

Publisher: American Society of Mechanical Engineers

Paper No: 97-GT-124

https://doi.org/10.1115/97-GT-124

View Paper titled, A Three-Dimensional Turbine Engine Analysis Compressor Code (TEACC) for Steady-State Inlet Distortion

Topics: Compressors, Gas turbines, Steady state, Blades, Rotors, Design, Flow (Dynamics), Modeling, NASA, Rotation

Proceedings Papers

An Argument for Enhancement of the Current Inlet Distortion Ground Test Practice for Aircraft Gas Turbine Engines

Milt Davis, Alan Hale, Dave Beale

Proc. ASME. GT2001, Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery, V001T01A011, June 4–7, 2001

Publisher: American Society of Mechanical Engineers

Paper No: 2001-GT-0507

https://doi.org/10.1115/2001-GT-0507

View Paper titled, An Argument for Enhancement of the Current Inlet Distortion Ground Test Practice for Aircraft Gas Turbine Engines

Topics: Aircraft, Gas turbines, Engines, Pressure, Simulation, Stability, Compression, Flow (Dynamics), Industrial research, Propulsion

Proceedings Papers

An Investigation Into the Effects of Highly Transient Flight Maneuvers With Heat and Mass Transfer on the T-38 Air Force Trainer Inlet

Alan Hale, Andrew Hughes, Jim Sirbaugh, David S. Kidman

Proc. ASME. GT2010, Volume 1: Aircraft Engine; Ceramics; Coal, Biomass and Alternative Fuels; Education; Electric Power; Manufacturing Materials and Metallurgy, 275-285, June 14–18, 2010

Publisher: American Society of Mechanical Engineers

Paper No: GT2010-22829

https://doi.org/10.1115/GT2010-22829

View Paper titled, An Investigation Into the Effects of Highly Transient Flight Maneuvers With Heat and Mass Transfer on the T-38 Air Force Trainer Inlet

Topics: Air Force, Flight, Heat, Mass transfer, Transients (Dynamics), Engines, Flow (Dynamics), Temperature, Computational fluid dynamics, Stability

Journal Articles

An Investigation Into the Effects of Highly Transient Flight Maneuvers With Heat and Mass Transfer on the T-38 Air Force Trainer Inlet

Alan Hale, Andrew Hughes, Jim Sirbaugh, David S. Kidman

Publisher: ASME

J. Eng. Gas Turbines Power. March 2011, 133(3): 031201.

https://doi.org/10.1115/1.4001995

Published Online: November 12, 2010

View Article titled, An Investigation Into the Effects of Highly Transient Flight Maneuvers With Heat and Mass Transfer on the T-38 Air Force Trainer Inlet

Topics: Boundary layers, Computational fluid dynamics, Engines, Flight, Temperature, Transients (Dynamics), Heat transfer, Heat, Mass transfer, Aircraft

Proceedings Papers

A Parametric Study on the Effects of Inlet Swirl on Compression System Performance and Operability Using Numerical Simulations

Milt Davis, Alan Hale

Proc. ASME. GT2007, Volume 1: Turbo Expo 2007, 1-10, May 14–17, 2007

Publisher: American Society of Mechanical Engineers

Paper No: GT2007-27033

https://doi.org/10.1115/GT2007-27033

View Paper titled, A Parametric Study on the Effects of Inlet Swirl on Compression System Performance and Operability Using Numerical Simulations

Topics: Compression, Computer simulation, Flow (Dynamics), Engines, Design, Pressure, Compressors, Engineering disciplines, Gas turbines, Military aircraft

Proceedings Papers

A Numerical Simulation Capability for Analysis of Aircraft Inlet – Engine Compatibility

Alan Hale, Milt Davis, Jim Sirbaugh

Proc. ASME. GT2004, Volume 2: Turbo Expo 2004, 127-137, June 14–17, 2004

Publisher: American Society of Mechanical Engineers

Paper No: GT2004-53473

https://doi.org/10.1115/GT2004-53473

View Paper titled, A Numerical Simulation Capability for Analysis of Aircraft Inlet – Engine Compatibility

Topics: Aircraft, Computer simulation, Engines, Military systems, Aircraft propulsion, Compressors, Flight, Gas turbines

Proceedings Papers

A Numerical Investigation of the Effects of Steam Ingestion on Compression System Performance

Jason Klepper, Alan Hale, Milt Davis, Wayne Hurwitz

Proc. ASME. GT2004, Volume 2: Turbo Expo 2004, 295-303, June 14–17, 2004

Publisher: American Society of Mechanical Engineers

Paper No: GT2004-54190

https://doi.org/10.1115/GT2004-54190

View Paper titled, A Numerical Investigation of the Effects of Steam Ingestion on Compression System Performance

Topics: Compression, Steam, Gas turbines, Water, Blades, Compressors, Constants (Physics), Engineering standards, Fluids, Heat transfer

Proceedings Papers

A Numerical Capability to Analyze the Effects of Water Ingestion on Compression System Performance and Operability

Alan Hale, Jason Klepper, Wayne Hurwitz

Proc. ASME. GT2005, Volume 1: Turbo Expo 2005, 113-125, June 6–9, 2005

Publisher: American Society of Mechanical Engineers

Paper No: GT2005-68480

https://doi.org/10.1115/GT2005-68480

View Paper titled, A Numerical Capability to Analyze the Effects of Water Ingestion on Compression System Performance and Operability

Topics: Compression, Water, Compressors, Heat transfer, Aircraft, Cycles, Flow (Dynamics), Industrial gases, Modeling, Simulation

Journal Articles

A Numerical Simulation Capability for Analysis of Aircraft Inlet-Engine Compatibility

Alan Hale, Milt Davis, Jim Sirbaugh

Publisher: ASME

J. Eng. Gas Turbines Power. July 2006, 128(3): 473–481.

https://doi.org/10.1115/1.1925649

Published Online: March 1, 2004

View Article titled, A Numerical Simulation Capability for Analysis of Aircraft Inlet-Engine Compatibility

Topics: Aircraft, Compression, Compressors, Computer simulation, Engines, Flow (Dynamics), Military systems, Pressure, Simulation, Steady state

Journal Articles

An Argument for Enhancement of the Current Inlet Distortion Ground Test Practice for Aircraft Gas Turbine Engines

Milt Davis, Alan Hale, Dave Beale

Publisher: ASME

J. Turbomach. April 2002, 124(2): 235–241.

https://doi.org/10.1115/1.1451087

Published Online: April 9, 2002

View Article titled, An Argument for Enhancement of the Current Inlet Distortion Ground Test Practice for Aircraft Gas Turbine Engines

Topics: Aircraft, Compressors, Engines, Flow (Dynamics), Gas turbines, Pressure, Rotation, Rotors, Simulation, Stability

Journal citation

NARROW

A Three-Dimensional Turbine Engine Analysis Compressor Code (TEACC) for Steady-State Inlet Distortion

An Argument for Enhancement of the Current Inlet Distortion Ground Test Practice for Aircraft Gas Turbine Engines

An Investigation Into the Effects of Highly Transient Flight Maneuvers With Heat and Mass Transfer on the T-38 Air Force Trainer Inlet

An Investigation Into the Effects of Highly Transient Flight Maneuvers With Heat and Mass Transfer on the T-38 Air Force Trainer Inlet

A Parametric Study on the Effects of Inlet Swirl on Compression System Performance and Operability Using Numerical Simulations

A Numerical Simulation Capability for Analysis of Aircraft Inlet – Engine Compatibility

A Numerical Investigation of the Effects of Steam Ingestion on Compression System Performance

A Numerical Capability to Analyze the Effects of Water Ingestion on Compression System Performance and Operability

A Numerical Simulation Capability for Analysis of Aircraft Inlet-Engine Compatibility

An Argument for Enhancement of the Current Inlet Distortion Ground Test Practice for Aircraft Gas Turbine Engines

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