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Journal Articles

A Method for Predicting the Aeroelastic Response of Radial Turbomachines

David Fellows, Vincent Iskandar, Daniel Bodony, Ryan C. McGowan, Sang-Guk Kang, Aaron J. Pope, Chol-Bum M. Kweon

J. Turbomach.

Paper No: TURBO-22-1117

DOI: https://doi.org/10.1115/1.4057062

Published Online: March 8, 2023

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Topics: Computational fluid dynamics, Turbine blades, Turbochargers, Turbomachinery, Flutter (Aerodynamics), Blades, Fluids, Turbines, Aircraft, Combustion

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

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

Paper No: TURBO-21-1308

DOI: https://doi.org/10.1115/1.4054035

Published Online: April 7, 2022

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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

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

Paper No: TURBO-12-1250

DOI: https://doi.org/10.1115/1.4023908

Published Online: September 26, 2013

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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

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

DOI: https://doi.org/10.1115/1.4003072

Published Online: July 15, 2011

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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

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

DOI: https://doi.org/10.1115/1.4003223

Published Online: May 24, 2011

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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

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

DOI: https://doi.org/10.1115/1.4001221

Published Online: May 11, 2010

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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

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

DOI: https://doi.org/10.1115/1.3192145

Published Online: April 26, 2010

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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

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

DOI: https://doi.org/10.1115/1.2992515

Published Online: April 20, 2009

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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

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

DOI: https://doi.org/10.1115/1.2372768

Published Online: January 1, 2007

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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

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

DOI: https://doi.org/10.1115/1.2472398

Published Online: July 23, 2006

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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

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

DOI: https://doi.org/10.1115/1.2372779

Published Online: February 1, 2006

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

Journal Articles

The Jet Age, Continued

William H. Heiser

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

DOI: https://doi.org/10.1115/1.1791278

Published Online: February 9, 2005

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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

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

DOI: https://doi.org/10.1115/1.1452246

Published Online: April 9, 2002

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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

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 Articles

Performance Assessment of an Annular S-Shaped Duct

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

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

DOI: https://doi.org/10.1115/1.2841003

Published Online: January 1, 1997

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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

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

DOI: https://doi.org/10.1115/1.2929291

Published Online: July 1, 1993

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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

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

DOI: https://doi.org/10.1115/1.2929141

Published Online: April 1, 1992

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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

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

DOI: https://doi.org/10.1115/1.2927695

Published Online: October 1, 1990

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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

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

DOI: https://doi.org/10.1115/1.3262280

Published Online: October 1, 1989

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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

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

DOI: https://doi.org/10.1115/1.3262154

Published Online: January 1, 1988

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

Journal citation

NARROW

Manuscript

A Method for Predicting the Aeroelastic Response of Radial Turbomachines

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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