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Journal Articles

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

Zhibo Chen, Marshall C. Galbraith, Zoltán S. Spakovszky, Edward M. Greitzer, Jayant S. Sabnis

Publisher: ASME

J. Turbomach. February 2024, 146(2): 021004.

Paper No: TURBO-23-1234

https://doi.org/10.1115/1.4063930

Published Online: November 8, 2023

View Article titled, Tail-Integrated Boundary Layer Ingesting Propulsion Systems for Turbo-Electric Aircraft

Topics: Aircraft, Boundary layers, Design, Flow (Dynamics), Nozzles, Propulsion systems, Mach number

Journal Articles

Inlet Flow Distortion in an Advanced Civil Transport Boundary Layer Ingesting Engine Installation

D. K. Hall, E. M. Greitzer, A. Uranga, M. Drela, S. A. Pandya

Publisher: ASME

J. Turbomach. October 2022, 144(10): 101002.

Paper No: TURBO-21-1308

https://doi.org/10.1115/1.4054035

Published Online: April 7, 2022

View Article titled, Inlet Flow Distortion in an Advanced Civil Transport Boundary Layer Ingesting Engine Installation

Topics: Aircraft, Boundary layers, Flow (Dynamics), Pressure, Computation, Engines

Journal Articles

Drag Management in High Bypass Turbofan Nozzles for Quiet Approach Applications

P. Shah, A. Robinson, A. Price, Z. Spakovszky

Publisher: ASME

J. Turbomach. February 2014, 136(2): 021009.

Paper No: TURBO-12-1250

https://doi.org/10.1115/1.4023908

Published Online: September 26, 2013

View Article titled, Drag Management in High Bypass Turbofan Nozzles for Quiet Approach Applications

Topics: Drag (Fluid dynamics), Flow (Dynamics), Noise (Sound), Nozzles, Swirling flow, Simulation, Engines, Computational fluid dynamics, Aircraft

Journal Articles

Minimizing Inlet Distortion for Hybrid Wing Body Aircraft

Meng-Sing Liou, Byung Joon Lee

Publisher: ASME

J. Turbomach. May 2012, 134(3): 031020.

https://doi.org/10.1115/1.4003072

Published Online: July 15, 2011

View Article titled, Minimizing Inlet Distortion for Hybrid Wing Body Aircraft

Topics: Boundary layers, Design, Flow (Dynamics), Geometry, Optimization, Pressure, Aircraft, Wings, Shapes

Journal Articles

Rotor Interaction Noise in Counter-Rotating Propfan Propulsion Systems

Andreas Peters, Zoltán S. Spakovszky

Publisher: ASME

J. Turbomach. January 2012, 134(1): 011002.

https://doi.org/10.1115/1.4003223

Published Online: May 24, 2011

View Article titled, Rotor Interaction Noise in Counter-Rotating Propfan Propulsion Systems

Topics: Carbon reinforced plastics, Design, Noise (Sound), Rotors, Aircraft, Acoustics, Blades

Journal Articles

Preparing for the Future: Reducing Gas Turbine Environmental Impact—IGTI Scholar Lecture

Nicholas A. Cumpsty

Publisher: ASME

J. Turbomach. October 2010, 132(4): 041017.

https://doi.org/10.1115/1.4001221

Published Online: May 11, 2010

View Article titled, Preparing for the Future: Reducing Gas Turbine Environmental Impact—IGTI Scholar Lecture

Topics: Aircraft, Design, Engines, Fuels, Gas turbines, Pressure, Temperature, Thrust, Turbines, Flow (Dynamics)

Journal Articles

A Novel Turbomachinery Air-Brake Concept for Quiet Aircraft

P. N. Shah, D. D. Mobed, Z. S. Spakovszky

Publisher: ASME

J. Turbomach. October 2010, 132(4): 041002.

https://doi.org/10.1115/1.3192145

Published Online: April 26, 2010

View Article titled, A Novel Turbomachinery Air-Brake Concept for Quiet Aircraft

Topics: Acoustics, Aircraft, Brakes, Design, Drag (Fluid dynamics), Ducts, Flow (Dynamics), Noise (Sound), Pressure, Swirling flow

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

Journal Articles

Online Water Wash Tests of GE J85-13

Elisabet Syverud, Lars E. Bakken

Publisher: ASME

J. Turbomach. January 2007, 129(1): 136–142.

https://doi.org/10.1115/1.2372768

Published Online: January 1, 2007

View Article titled, Online Water Wash Tests of GE J85-13

Topics: Compressors, Jet engines, Test facilities, Water, Engines, Aerospace industry, Drops, Air Force, Aircraft, Instrumentation

Journal Articles

Engine Design Studies for a Silent Aircraft

Cesare A. Hall, Daniel Crichton

Publisher: ASME

J. Turbomach. July 2007, 129(3): 479–487.

https://doi.org/10.1115/1.2472398

Published Online: July 23, 2006

View Article titled, Engine Design Studies for a Silent Aircraft

Topics: Aircraft, Cycles, Design, Engines, Noise (Sound), Turbofans, Propulsion systems, Nozzles, Exhaust systems, Thrust

Journal Articles

Preliminary Fan Design for a Silent Aircraft

Daniel Crichton, Liping Xu, Cesare A. Hall

Publisher: ASME

J. Turbomach. January 2007, 129(1): 184–191.

https://doi.org/10.1115/1.2372779

Published Online: February 1, 2006

View Article titled, Preliminary Fan Design for a Silent Aircraft

Topics: Aircraft, Design, Engines, Noise (Sound), Nozzles, Pressure, Rotors, Flow (Dynamics), Overpasses, Mach number

Journal Articles

The Jet Age, Continued

William H. Heiser

Publisher: ASME

J. Turbomach. January 2005, 127(1): 2–4.

https://doi.org/10.1115/1.1791278

Published Online: February 9, 2005

View Article titled, The Jet Age, Continued

Topics: Aircraft, Cycles, Engines, Jet engines, Propulsion, Turbines, Design, Fuels, Gas turbines, Aerospace industry

Journal Articles

Turbine Engine Performance Improvements—A Proactive Approach

Zane D. Gastineau

Publisher: ASME

J. Turbomach. April 2002, 124(2): 223–226.

https://doi.org/10.1115/1.1452246

Published Online: April 9, 2002

View Article titled, Turbine Engine Performance Improvements—A Proactive Approach

Topics: Engines, Gas turbines, Stability, Design, Control systems, Aircraft

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 Articles

Performance Assessment of an Annular S-Shaped Duct

D. W. Bailey, K. M. Britchford, J. F. Carrote, S. J. Stevens

Publisher: ASME

J. Turbomach. January 1997, 119(1): 149–156.

https://doi.org/10.1115/1.2841003

Published Online: January 1, 1997

View Article titled, Performance Assessment of an Annular S-Shaped Duct

Topics: Ducts, Compressors, Pressure, Engines, Flow (Dynamics), Shear stress, Struts (Engineering), Aircraft, Blades, Boundary layers

Journal Articles

Design and Rotor Performance of a 5:1 Mixed-Flow Supersonic Compressor

R. Mo¨nig, W. Elmendorf, H. E. Gallus

Publisher: ASME

J. Turbomach. July 1993, 115(3): 565–572.

https://doi.org/10.1115/1.2929291

Published Online: July 1, 1993

View Article titled, Design and Rotor Performance of a 5:1 Mixed-Flow Supersonic Compressor

Topics: Compressors, Design, Flow (Dynamics), Rotors, Stators, Shock waves, Aircraft, Engines, High pressure (Physics), Jet engines

Journal Articles

Design of a High-Performance Axial Compressor for Utility Gas Turbine

A. Sehra, J. Bettner, A. Cohn

Publisher: ASME

J. Turbomach. April 1992, 114(2): 277–286.

https://doi.org/10.1115/1.2929141

Published Online: April 1, 1992

View Article titled, Design of a High-Performance Axial Compressor for Utility Gas Turbine

Topics: Compressors, Design, Gas turbines, Flow (Dynamics), Geometry, Inlet guide vanes, Stators, Aircraft, Aircraft engines, Airfoils

Journal Articles

Highly Loaded Axial Flow Compressors: History and Current Developments

A. J. Wennerstrom

Publisher: ASME

J. Turbomach. October 1990, 112(4): 567–578.

https://doi.org/10.1115/1.2927695

Published Online: October 1, 1990

View Article titled, Highly Loaded Axial Flow Compressors: History and Current Developments

Topics: Axial flow, Compressors, Diffusion (Physics), Mach number, Aircraft, Gas turbines, Power stations, Weight (Mass)

Journal Articles

Low Aspect Ratio Axial Flow Compressors: Why and What It Means

A. J. Wennerstrom

Publisher: ASME

J. Turbomach. October 1989, 111(4): 357–365.

https://doi.org/10.1115/1.3262280

Published Online: October 1, 1989

View Article titled, Low Aspect Ratio Axial Flow Compressors: Why and What It Means

Topics: Axial flow, Compressors, Design, Aircraft, Design engineering, Engines, Gas turbines, Fans, Pendulums, Stability

Journal Articles

Aerodynamic Design of a Power Turbine for an Aircraft Derivative Marine Gas Turbine

Guiming Ji, Zengxiang Tan, Mingchang Zhang

Publisher: ASME

J. Turbomach. January 1988, 110(1): 104–109.

https://doi.org/10.1115/1.3262154

Published Online: January 1, 1988

View Article titled, Aerodynamic Design of a Power Turbine for an Aircraft Derivative Marine Gas Turbine

Topics: Aircraft, Design, Marine gas turbines, Turbines, Equilibrium (Physics), Blades, Design methodology, Flow (Dynamics), Generators, Geometry

Journal citation

NARROW

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

Inlet Flow Distortion in an Advanced Civil Transport Boundary Layer Ingesting Engine Installation

Drag Management in High Bypass Turbofan Nozzles for Quiet Approach Applications

Minimizing Inlet Distortion for Hybrid Wing Body Aircraft

Rotor Interaction Noise in Counter-Rotating Propfan Propulsion Systems

Preparing for the Future: Reducing Gas Turbine Environmental Impact—IGTI Scholar Lecture

A Novel Turbomachinery Air-Brake Concept for Quiet Aircraft

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

Online Water Wash Tests of GE J85-13

Engine Design Studies for a Silent Aircraft

Preliminary Fan Design for a Silent Aircraft

The Jet Age, Continued

Turbine Engine Performance Improvements—A Proactive Approach

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

Performance Assessment of an Annular S-Shaped Duct

Design and Rotor Performance of a 5:1 Mixed-Flow Supersonic Compressor

Design of a High-Performance Axial Compressor for Utility Gas Turbine

Highly Loaded Axial Flow Compressors: History and Current Developments

Low Aspect Ratio Axial Flow Compressors: Why and What It Means

Aerodynamic Design of a Power Turbine for an Aircraft Derivative Marine Gas Turbine

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