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Proceedings Papers

An Approach for the Development of an Aerodynamic-Structural Interaction Numerical Simulation for Aeropropulsion Systems

Proc. ASME. GT1996, Volume 5: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; General, V005T16A019, June 10–13, 1996

Paper No: 96-GT-480

DOI: https://doi.org/10.1115/96-GT-480

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Topics: Computer simulation, Simulation, Turbomachinery, Combustion chambers, Compressors, Design, Fluids, Aerospace industry, Compression, Flight

Proceedings Papers

A One Dimensional, Time Dependent Inlet / Engine Numerical Simulation for Aircraft Propulsion Systems

Doug Garrard, Milt Davis, Jr., Steve Wehofer, Gary Cole

Proc. ASME. GT1997, Volume 4: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; IGTI Scholar Award, V004T16A010, June 2–5, 1997

Paper No: 97-GT-333

DOI: https://doi.org/10.1115/97-GT-333

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Topics: Aircraft propulsion, Computer simulation, Engines, Gas turbines, Flow (Dynamics), Simulation, Compressors, Computers, Momentum, NASA

Proceedings Papers

A Proposal for Integration of Wind Tunnel and Engine Test Programs for the Evaluation of Airframe-Propulsion Compatibility Using Numerical Simulations

Milt Davis, William Baker, Greg Power, Dave Beale

Proc. ASME. GT1999, Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery, V001T01A008, June 7–10, 1999

Paper No: 99-GT-345

DOI: https://doi.org/10.1115/99-GT-345

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Topics: Computer simulation, Engines, Propulsion, Wind tunnels, Aircraft, Industrial research, Navier-Stokes equations, Propulsion systems, Testing

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

Paper No: 2001-GT-0507

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

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

Proceedings Papers

Investigation of the Effects of Inlet Swirl on Compressor Performance and Operability Using a Modified Parallel Compressor Model

Nicholas Fredrick, Milt Davis, Jr.

Proc. ASME. GT2011, Volume 1: Aircraft Engine; Ceramics; Coal, Biomass and Alternative Fuels; Wind Turbine Technology, 177-187, June 6–10, 2011

Paper No: GT2011-45553

DOI: https://doi.org/10.1115/GT2011-45553

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Topics: Compressors, Engines, Pressure, Testing, Aircraft, Gas turbines, Inlet guide vanes, Propulsion systems, Turbofans, Blades

Proceedings Papers

Integrated Test and Evaluation Techniques as Applied to an Inlet Swirl Investigation Using the F109 Gas Turbine Engine

Milt Davis, Dave Beale, Yogi Sheoran

Proc. ASME. GT2008, Volume 1: Aircraft Engine; Ceramics; Coal, Biomass and Alternative Fuels; Manufacturing, Materials and Metallurgy; Microturbines and Small Turbomachinery, 9-20, June 9–13, 2008

Paper No: GT2008-50074

DOI: https://doi.org/10.1115/GT2008-50074

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Topics: Gas turbines, Aerospace systems, Air Force, Compressors, Computer simulation, Decision making, Design, Engines, Flight, Risk management

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

Paper No: GT2007-27033

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

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

Proceedings Papers

A Flight Simulation Vision for Aeropropulsion Altitude Ground Test Facilities

Milt Davis, Peter Montgomery

Proc. ASME. GT2002, Volume 1: Turbo Expo 2002, 21-31, June 3–6, 2002

Paper No: GT2002-30003

DOI: https://doi.org/10.1115/GT2002-30003

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Topics: Flight, Simulation, Test facilities, Aircraft, Engines, Testing, Instrumentation, Propulsion systems, Air flow, Aircraft engines

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

Paper No: GT2004-53473

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

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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

Paper No: GT2004-54190

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

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

Proceedings Papers

Requirements and Advances in Simulating Aircraft Inlet Total Pressure Distortion in Turbine Engine Ground Tests

Dave Beale, Milt Davis, Jim Sirbaugh

Proc. ASME. GT2006, Volume 2: Aircraft Engine; Ceramics; Coal, Biomass and Alternative Fuels; Controls, Diagnostics and Instrumentation; Environmental and Regulatory Affairs, 25-36, May 8–11, 2006

Paper No: GT2006-90038

DOI: https://doi.org/10.1115/GT2006-90038

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Topics: Aircraft, Gas turbines, Pressure, Generators, Computational fluid dynamics, Engineering prototypes, Engines, Simulation, Control systems, Design

Journal Articles

A Flight Simulation Vision for Aeropropulsion Altitude Ground Test Facilities

Milt Davis, Peter Montgomery

J. Eng. Gas Turbines Power. January 2005, 127(1): 8–17.

DOI: https://doi.org/10.1115/1.1806452

Published Online: February 9, 2005

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Topics: Aircraft, Engines, Flight, Simulation, Test facilities, Flow (Dynamics)

Journal Articles

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

Alan Hale, Milt Davis, Jim Sirbaugh

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

DOI: https://doi.org/10.1115/1.1925649

Published Online: March 1, 2004

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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

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

DOI: https://doi.org/10.1115/1.1451087

Published Online: April 9, 2002

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

Journal citation

NARROW

An Approach for the Development of an Aerodynamic-Structural Interaction Numerical Simulation for Aeropropulsion Systems

A One Dimensional, Time Dependent Inlet / Engine Numerical Simulation for Aircraft Propulsion Systems

A Proposal for Integration of Wind Tunnel and Engine Test Programs for the Evaluation of Airframe-Propulsion Compatibility Using Numerical Simulations

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

Investigation of the Effects of Inlet Swirl on Compressor Performance and Operability Using a Modified Parallel Compressor Model

Integrated Test and Evaluation Techniques as Applied to an Inlet Swirl Investigation Using the F109 Gas Turbine Engine

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

A Flight Simulation Vision for Aeropropulsion Altitude Ground Test Facilities

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

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

Requirements and Advances in Simulating Aircraft Inlet Total Pressure Distortion in Turbine Engine Ground Tests

A Flight Simulation Vision for Aeropropulsion Altitude Ground Test Facilities

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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