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Journal Articles

Investigation of Riblet Geometry and Start Locations of Herringbone Riblets on Pressure Losses in a Linear Cascade at Low Reynolds Numbers

Qiang Liu, Shan Zhong, Lin Li
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach. October 2020, 142(10): 101010.
Paper No: TURBO-19-1090
https://doi.org/10.1115/1.4046960
Published Online: September 16, 2020
View Article titled, Investigation of Riblet Geometry and Start Locations of Herringbone Riblets on Pressure Losses in a Linear Cascade at Low Reynolds Numbers
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Topics: Blades, Cascades (Fluid dynamics), Flow (Dynamics), Flow separation, Geometry, Pressure, Reynolds number, Wakes, Flow turning, Boundary layers
Journal Articles

Multipoint optimization of an axial turbine cascade using a hybrid algorithm

Accepted Manuscript
Arnaud Châtel, Tom Verstraete, Grégory Coussement
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach.
Paper No: TURBO-19-1284
https://doi.org/10.1115/1.4046231
Published Online: February 5, 2020
View Article titled, Multipoint optimization of an axial turbine cascade using a hybrid algorithm
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Topics: Algorithms, Cascades (Fluid dynamics), Design, Optimization, Turbines, Turbochargers, Entropy, Evolutionary algorithms, Flow (Dynamics), Blades
Journal Articles

Effects of Bio-Inspired Micro-Scale Surface Patterns on the Profile Losses in a Linear Cascade

Qiang Liu, Shan Zhong, Lin Li
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach. December 2019, 141(12): 121006.
Paper No: TURBO-19-1069
https://doi.org/10.1115/1.4044612
Published Online: November 21, 2019
View Article titled, Effects of Bio-Inspired Micro-Scale Surface Patterns on the Profile Losses in a Linear Cascade
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Topics: Blades, Boundary layers, Cascades (Fluid dynamics), Flow (Dynamics), Flow turning, Pressure, Wakes, Suction, Flow separation, Compressors
Journal Articles

Numerical and Experimental Comparison of a Tandem and Single Vane Deswirler Used in an Aero Engine Centrifugal Compressor

Benjamin Wilkosz, Johannes Schmidt, Christian Guenther, Philipp Schwarz, Peter Jeschke, Caitlin Smythe
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research-Article
J. Turbomach. April 2014, 136(4): 041005.
Paper No: TURBO-13-1067
https://doi.org/10.1115/1.4024891
Published Online: September 26, 2013
View Article titled, Numerical and Experimental Comparison of a Tandem and Single Vane Deswirler Used in an Aero Engine Centrifugal Compressor
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Topics: Aircraft engines, Blades, Boundary layers, Compressors, Design, Diffusers, Diffusion (Physics), Flow (Dynamics), Pressure, Flow turning
Journal Articles

Numerical and Experimental Investigation of Turning Flow Effects on Innovative Pin Fin Arrangements for Trailing Edge Cooling Configurations

C. Bianchini, B. Facchini, F. Simonetti, L. Tarchi, S. Zecchi
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach. March 2012, 134(2): 021005.
https://doi.org/10.1115/1.4003230
Published Online: June 22, 2011
View Article titled, Numerical and Experimental Investigation of Turning Flow Effects on Innovative Pin Fin Arrangements for Trailing Edge Cooling Configurations
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Topics: Blades, Cooling, Ducts, Fins, Flow (Dynamics), Heat transfer, Heat transfer coefficients, Pins (Engineering), Pressure, Turbulence
Journal Articles

1999 Turbomachinery Committee Best Paper Award: Development of Advanced Compressor Airfoils for Heavy-Duty Gas Turbines— Part II: Experimental and Theoretical Analysis

Bernhard Ku¨sters, Heinz-Adolf Schreiber, Ulf Ko¨ller, Reinhard Mo¨nig
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Technical Papers
J. Turbomach. July 2000, 122(3): 406–414.
https://doi.org/10.1115/1.1302321
Published Online: February 1, 1999
View Article titled, 1999 Turbomachinery Committee Best Paper Award: Development of Advanced Compressor Airfoils for Heavy-Duty Gas Turbines— Part II: Experimental and Theoretical Analysis
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Topics: Blades, Boundary layers, Cascades (Fluid dynamics), Compressors, Design, Flow (Dynamics), Gas turbines, Mach number, Pressure, Reynolds number
Journal Articles

An Investigation of a Strong Shock-Wave Turbulent Boundary Layer Interaction in a Supersonic Compressor Cascade

H. A. Schreiber, H. Starken
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach. July 1992, 114(3): 494–503.
https://doi.org/10.1115/1.2929170
Published Online: July 1, 1992
View Article titled, An Investigation of a Strong Shock-Wave Turbulent Boundary Layer Interaction in a Supersonic Compressor Cascade
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Topics: Boundary layer turbulence, Cascades (Fluid dynamics), Compressors, Shock waves, Blades, Mach number, Pressure, Boundary layers, Chords (Trusses), Density