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Journal Articles

Experimental and Numerical Similitude Study Using a Novel Turbocompressor Test Facility Operating With Helium–Neon Gas Mixtures

Maxime Podeur, Damian M. Vogt

J. Turbomach. August 2022, 144(8): 081015.

Paper No: TURBO-21-1213

DOI: https://doi.org/10.1115/1.4053987

Published Online: March 16, 2022

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Topics: Compressors, Design, Heat transfer, Mach number, Pressure, Reynolds number, Specific heat, Helium, Test facilities, Temperature

Journal Articles

Effect of Tip Vortex Reduction on Air-Cooled Condenser Axial Flow Fan Performance: An Experimental Investigation

Johannes P. Pretorius, Johan A. Erasmus

J. Turbomach. March 2022, 144(3): 031001.

Paper No: TURBO-21-1152

DOI: https://doi.org/10.1115/1.4052234

Published Online: September 29, 2021

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Topics: Axial flow, Blades, Clearances (Engineering), Flow (Dynamics), Pressure, Test facilities, Testing, Wake turbulence, Condensers (steam plant), Design

Journal Articles

Aerodynamic Investigation of a Composite Low-Speed Fan for UHBR Application

Martin Rodrigues, Laurent Soulat, Benoit Paoletti, Xavier Ottavy, Christoph Brandstetter

J. Turbomach. October 2021, 143(10): 101004.

Paper No: TURBO-20-1413

DOI: https://doi.org/10.1115/1.4050671

Published Online: May 12, 2021

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Topics: Blades, Composite materials, Design, Flow (Dynamics), Leakage, Pressure, Reynolds-averaged Navier–Stokes equations, Rotors, Simulation, Turbulence

Journal Articles

Wall Temperature Measurements in a Full-Scale Gas Turbine Combustor Test Rig With Fiber Coupled Phosphor Thermometry

Patrick Nau, Simon Görs, Christoph Arndt, Benjamin Witzel, Torsten Endres

J. Turbomach. January 2021, 143(1): 011007.

Paper No: TURBO-20-1229

DOI: https://doi.org/10.1115/1.4049104

Published Online: December 28, 2020

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Topics: Combustion chambers, Emissions, Fibers, Gas turbines, Lasers, Phosphors, Probes, Signals, Temperature, Temperature measurement

Journal Articles

Project PHARE-2—A High-Speed UHBR Fan Test Facility for a New Open-Test Case

Christoph Brandstetter, Valdo Pages, Pierre Duquesne, Benoit Paoletti, Stéphane Aubert, Xavier Ottavy

J. Turbomach. October 2019, 141(10): 101004.

Paper No: TURBO-18-1311

DOI: https://doi.org/10.1115/1.4043883

Published Online: September 23, 2019

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Topics: Design, Rotors, Test facilities, Blades, Geometry, Acoustics

Journal Articles

Experimental Investigation of an Aerodynamically Mistuned Oscillating Compressor Cascade

Leonie Malzacher, Christopher Schwarze, Valentina Motta, Dieter Peitsch

J. Turbomach. July 2019, 141(7): 071012.

Paper No: TURBO-19-1027

DOI: https://doi.org/10.1115/1.4043474

Published Online: May 23, 2019

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Topics: Blades, Cascades (Fluid dynamics), Compressors, Damping, Pressure, Stability, Test facilities, Flow (Dynamics), Aerodynamics

Journal Articles

A New Test Facility to Investigate Film Cooling on a Nonaxisymmetric Contoured Turbine Endwall—Part II: Heat Transfer and Film Cooling Measurements

Johannes Kneer, Franz Puetz, Achmed Schulz, Hans-Jörg Bauer

J. Turbomach. July 2016, 138(7): 071004.

Paper No: TURBO-15-1266

DOI: https://doi.org/10.1115/1.4032364

Published Online: February 17, 2016

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Topics: Film cooling, Heat transfer, Temperature, Turbines, Coolants, Test facilities

Journal Articles

Turbine Efficiency Measurement System for the QinetiQ Turbine Test Facility

Paul F. Beard, Thomas Povey, Kamaljit S. Chana

J. Turbomach. January 2010, 132(1): 011002.

DOI: https://doi.org/10.1115/1.3066271

Published Online: September 11, 2009

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Topics: Calibration, Flow (Dynamics), Pressure, Temperature, Torque, Turbines, Uncertainty, Strain gages, Test facilities, Rotors

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

Simulated Land-Based Turbine Deposits Generated in an Accelerated Deposition Facility

Jared W. Jensen, Sean W. Squire, Jeffrey P. Bons, Thomas H. Fletcher

J. Turbomach. July 2005, 127(3): 462–470.

DOI: https://doi.org/10.1115/1.1860380

Published Online: March 1, 2004

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Topics: Flow (Dynamics), Mach number, Particulate matter, Temperature, Turbine blades, Turbines, Blades, Gas turbines, Convection, Heat conduction

Journal Articles

Experimental Study of 3D Unsteady Flow Around Oscillating Blade With Part-Span Separation

O. J. R. Queune, L. He

J. Turbomach. July 2001, 123(3): 519–525.

DOI: https://doi.org/10.1115/1.1370164

Published Online: February 1, 2000

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Topics: Blades, Flow (Dynamics), Pressure, Pressure measurement, Separation (Technology), Test facilities, Unsteady flow, Flow separation, Turbine blades

Journal Articles

Computation and Measurement of the Flow in Axial Flow Fans With Skewed Blades

M. G. Beiler, T. H. Carolus

J. Turbomach. January 1999, 121(1): 59–66.

DOI: https://doi.org/10.1115/1.2841234

Published Online: January 1, 1999

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Topics: Axial flow, Blades, Computation, Fans, Flow (Dynamics), Pressure, Probes, Acoustics, Chords (Trusses), Design methodology

Journal Articles

Flowfield Measurements for Film-Cooling Holes With Expanded Exits

K. Thole, M. Gritsch, A. Schulz, S. Wittig

J. Turbomach. April 1998, 120(2): 327–336.

DOI: https://doi.org/10.1115/1.2841410

Published Online: April 1, 1998

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Topics: Film cooling, Cooling, Turbulence, Geometry, Mach number, Blades, Coolants, Density, Gas turbines, Shear (Mechanics)

Journal Articles

Three-Dimensional Unsteady Flow for an Oscillating Turbine Blade and the Influence of Tip Leakage

D. L. Bell, L. He

J. Turbomach. January 2000, 122(1): 93–101.

DOI: https://doi.org/10.1115/1.555432

Published Online: February 1, 1998

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Topics: Blades, Clearances (Engineering), Flow (Dynamics), Leakage, Pressure, Test facilities, Turbine blades, Unsteady flow, Leakage flows

Journal Articles

Flow Visualization and Leakage Measurements of Stepped Labyrinth Seals: Part 2—Sloping Surfaces

D. L. Rhode, J. S. Younger, M. D. Wernig

J. Turbomach. October 1997, 119(4): 844–848.

DOI: https://doi.org/10.1115/1.2841196

Published Online: October 1, 1997

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Topics: Flow visualization, Leakage, Geometry, Cavities, Dimensions, Flow (Dynamics), Rotors, Shapes, Test facilities, Turbulence

Journal Articles

Flow Visualization and Leakage Measurements of Stepped Labyrinth Seals: Part 1—Annular Groove

D. L. Rhode, J. W. Johnson, D. H. Broussard

J. Turbomach. October 1997, 119(4): 839–843.

DOI: https://doi.org/10.1115/1.2841195

Published Online: October 1, 1997

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Topics: Flow visualization, Leakage, Particulate matter, Stators, Test facilities, Water leakage

Journal Articles

Heat Transfer and Film Cooling Effectiveness in a Linear Airfoil Cascade

N. Abuaf, R. Bunker, C. P. Lee

J. Turbomach. April 1997, 119(2): 302–309.

DOI: https://doi.org/10.1115/1.2841113

Published Online: April 1, 1997

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Topics: Airfoils, Cascades (Fluid dynamics), Film cooling, Heat transfer, Heat transfer coefficients, Transients (Dynamics), Cylinders, Steady state, Boundary layers, Chords (Trusses)

Journal Articles

Transient Heat Transfer Experiments in a Linear Cascade Via an Insertion Mechanism Using the Liquid Crystal Technique

A. Hoffs, A. Bo¨lcs, S. P. Harasgama

J. Turbomach. January 1997, 119(1): 9–13.

DOI: https://doi.org/10.1115/1.2841016

Published Online: January 1, 1997

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Topics: Cascades (Fluid dynamics), Liquid crystals, Transient heat transfer, Airfoils, Boundary layers, Compressors, Displacement, Gages, Heat transfer, Image processing

Journal Articles

Performance Improvement Through Indexing of Turbine Airfoils: Part 1—Experimental Investigation

F. W. Huber, P. D. Johnson, O. P. Sharma, J. B. Staubach, S. W. Gaddis

J. Turbomach. October 1996, 118(4): 630–635.

DOI: https://doi.org/10.1115/1.2840918

Published Online: October 1, 1996

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Topics: Airfoils, Indexing (Machining), Turbines, Stators, Computational fluid dynamics, Testing, Design, Aeronautics, Computer simulation, Creeping flow

Journal Articles

Film Cooling With Compound Angle Holes: Adiabatic Effectiveness

D. L. Schmidt, B. Sen, D. G. Bogard

J. Turbomach. October 1996, 118(4): 807–813.

DOI: https://doi.org/10.1115/1.2840938

Published Online: October 1, 1996

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Topics: Film cooling, Momentum, Density, Coolants, Flat plates, Geometry, Pressure gradient, Test facilities

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Journal citation

NARROW

Experimental and Numerical Similitude Study Using a Novel Turbocompressor Test Facility Operating With Helium–Neon Gas Mixtures

Effect of Tip Vortex Reduction on Air-Cooled Condenser Axial Flow Fan Performance: An Experimental Investigation

Aerodynamic Investigation of a Composite Low-Speed Fan for UHBR Application

Wall Temperature Measurements in a Full-Scale Gas Turbine Combustor Test Rig With Fiber Coupled Phosphor Thermometry

Project PHARE-2—A High-Speed UHBR Fan Test Facility for a New Open-Test Case

Experimental Investigation of an Aerodynamically Mistuned Oscillating Compressor Cascade

A New Test Facility to Investigate Film Cooling on a Nonaxisymmetric Contoured Turbine Endwall—Part II: Heat Transfer and Film Cooling Measurements

Turbine Efficiency Measurement System for the QinetiQ Turbine Test Facility

Online Water Wash Tests of GE J85-13

Simulated Land-Based Turbine Deposits Generated in an Accelerated Deposition Facility

Experimental Study of 3D Unsteady Flow Around Oscillating Blade With Part-Span Separation

Computation and Measurement of the Flow in Axial Flow Fans With Skewed Blades

Flowfield Measurements for Film-Cooling Holes With Expanded Exits

Three-Dimensional Unsteady Flow for an Oscillating Turbine Blade and the Influence of Tip Leakage

Flow Visualization and Leakage Measurements of Stepped Labyrinth Seals: Part 2—Sloping Surfaces

Flow Visualization and Leakage Measurements of Stepped Labyrinth Seals: Part 1—Annular Groove

Heat Transfer and Film Cooling Effectiveness in a Linear Airfoil Cascade

Transient Heat Transfer Experiments in a Linear Cascade Via an Insertion Mechanism Using the Liquid Crystal Technique

Performance Improvement Through Indexing of Turbine Airfoils: Part 1—Experimental Investigation

Film Cooling With Compound Angle Holes: Adiabatic Effectiveness

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