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Journal Articles

Predicting Leidenfrost Temperature and Effects of Impact Conditions on Droplet Size Distribution in Film-Boiling Regime

Accepted Manuscript
Mohammad F.F. Patwary, Doruk Isik, Song-Charng Kong, Eric Mayhew, Kenneth Kim, Chol-Bum M. Kweon
Journal: Journal of Fluids Engineering
Publisher: ASME
Article Type: Research-Article
J. Fluids Eng.
Paper No: FE-24-1275
https://doi.org/10.1115/1.4066837
Published Online: October 14, 2024
View Article titled, Predicting Leidenfrost Temperature and Effects of Impact Conditions on Droplet Size Distribution in Film-Boiling Regime
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Journal Articles

Turbulent flow and wall forces in staggered square cylinder porous media: An LES Analysis

Accepted Manuscript
Oscar Morales-Contreras, Erik Herrera-Hernandez, Sergio Martinez-Delgadillo, Rene Sanjuan-Galindo, Norma Ramos, Alejandro Alonzo-Garcia
Journal: Journal of Fluids Engineering
Publisher: ASME
Article Type: Research-Article
J. Fluids Eng.
Paper No: FE-24-1292
https://doi.org/10.1115/1.4066836
Published Online: October 14, 2024
View Article titled, Turbulent flow and wall forces in staggered square cylinder porous media: An LES Analysis
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Journal Articles

Erratum: “Passively Enhanced Vortex-Induced Vibration Response of Side-by-Side Cylinders in Turbulent Flow” [ASME J. Fluids Eng., 2024, 146(7), p. 070903; DOI: 10.1115/1.4065302 ]

Yosua Heru Irawan, Syed Ahmad Raza, Ming-Jyh Chern
Journal: Journal of Fluids Engineering
Publisher: ASME
Article Type: Errata
J. Fluids Eng. December 2024, 146(12): 127001.
Paper No: FE-24-1410
https://doi.org/10.1115/1.4066484
Published Online: October 3, 2024
View Article titled, Erratum: “Passively Enhanced Vortex-Induced Vibration Response of Side-by-Side Cylinders in Turbulent Flow” [ASME J. Fluids Eng., 2024, 146(7), p. 070903; DOI: 10.1115/1.4065302 ]
Open the PDF for Erratum: “Passively Enhanced Vortex-Induced Vibration Response of Side-by-Side Cylinders in Turbulent Flow” [ASME J. Fluids Eng., 2024, 146(7), p. 070903; DOI: 10.1115/1.4065302 ] in another window
Topics: Cylinders, Fluids, Turbulence, Vortex-induced vibration
Journal Articles

Effect of Trailing Edge and Span Morphing on the Performance of an Optimized NACA6409 Wing in Ground Effect

Dominic Clements, Kamal Djidjeli
Journal: Journal of Fluids Engineering
Publisher: ASME
Article Type: Research-Article
J. Fluids Eng. January 2025, 147(1): 011206.
Paper No: FE-24-1133
https://doi.org/10.1115/1.4066487
Published Online: September 30, 2024
View Article titled, Effect of Trailing Edge and Span Morphing on the Performance of an Optimized NACA6409 Wing in Ground Effect
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Topics: Chords (Trusses), Drag (Fluid dynamics), Wings, Clearances (Engineering)
Journal Articles

Simulation of Interfacial Waves in Core-Annular Pipe Flow With a Turbulent Annulus

Haoyu Li, Mathieu Pourquié, Gijs Ooms, Ruud Henkes
Journal: Journal of Fluids Engineering
Publisher: ASME
Article Type: Research-Article
J. Fluids Eng. February 2025, 147(2): 021401.
Paper No: FE-24-1231
https://doi.org/10.1115/1.4066481
Published Online: September 30, 2024
View Article titled, Simulation of Interfacial Waves in Core-Annular Pipe Flow With a Turbulent Annulus
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Topics: Flow (Dynamics), Simulation, Turbulence, Water, Waves, Wavelength, Annulus, Pipes
Journal Articles

On Using the Distributor as a Multi Degree-of-Freedom System to Mitigate the Pressure Pulsation in an Axial Turbine at Speed-No-Load

Jelle Kranenbarg, Pontus P. Jonsson, Berhanu G. Mulu, Joel Sundström, Michel J. Cervantes
Journal: Journal of Fluids Engineering
Publisher: ASME
Article Type: Research-Article
J. Fluids Eng. February 2025, 147(2): 021501.
Paper No: FE-24-1254
https://doi.org/10.1115/1.4066482
Published Online: September 30, 2024
View Article titled, On Using the Distributor as a Multi Degree-of-Freedom System to Mitigate the Pressure Pulsation in an Axial Turbine at Speed-No-Load
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Topics: Blades, Computational fluid dynamics, Flow (Dynamics), Guide vanes, Machine learning, Pressure, Simulation, Turbines, Vortices, Stress
Journal Articles

Unified, Integral Approach to Modeling and Design of High-Pressure Pipelines: Assessment of Various Flow and Temperature Models for Supercritical Fluids

Guo-Xiang Wang, Vish Prasad
Journal: Journal of Fluids Engineering
Publisher: ASME
Article Type: Research-Article
J. Fluids Eng. February 2025, 147(2): 021402.
Paper No: FE-24-1298
https://doi.org/10.1115/1.4066483
Published Online: September 30, 2024
View Article titled, Unified, Integral Approach to Modeling and Design of High-Pressure Pipelines: Assessment of Various Flow and Temperature Models for Supercritical Fluids
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Topics: Flow (Dynamics), Fluids, Pipelines, Pipes, Pressure, Temperature
Journal Articles

Computational aeroacoustics of low-pressure axial fans installed in parallel

Accepted Manuscript
Debarshee Ghosh, Michail Vourakis, Niklas Andersson, Sassan Etemad
Journal: Journal of Fluids Engineering
Publisher: ASME
Article Type: Research-Article
J. Fluids Eng.
Paper No: FE-24-1304
https://doi.org/10.1115/1.4066752
Published Online: September 30, 2024
View Article titled, Computational aeroacoustics of low-pressure axial fans installed in parallel
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Topics: Aerodynamic noise, Fans, Pressure, Acoustics, Diffusion (Physics), Ducts, Electric vehicles, Engineering simulation, Simulation, Annulus
Journal Articles

Three-dimensional simulation of cavitating flow in reciprocating positive displacement pumps with fluid-actuated valves

Accepted Manuscript
Pascal Munsch, Joseph Kiermeir, Rudolf Schilling, Eberhard Schlücker, Romuald Skoda
Journal: Journal of Fluids Engineering
Publisher: ASME
Article Type: Research-Article
J. Fluids Eng.
Paper No: FE-24-1269
https://doi.org/10.1115/1.4066751
Published Online: September 30, 2024
View Article titled, Three-dimensional simulation of cavitating flow in reciprocating positive displacement pumps with fluid-actuated valves
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Topics: Flow (Dynamics), Fluids, Simulation, Vacuum pumps, Valves, Cavitation, Dynamics (Mechanics), Pressure, Algorithms, Collapse
Image
FishBAC concept [ 2 ]

FishBAC concept [ 2 ]

in Effect of Trailing Edge and Span Morphing on the Performance of an Optimized NACA6409 Wing in Ground Effect > Journal of Fluids Engineering
Published Online: September 30, 2024
Fig. 1 FishBAC concept [ 2 ] More about this image found in FishBAC concept [ 2 ]
Image
Input parameters for parametrization

Input parameters for parametrization

in Effect of Trailing Edge and Span Morphing on the Performance of an Optimized NACA6409 Wing in Ground Effect > Journal of Fluids Engineering
Published Online: September 30, 2024
Fig. 2 Input parameters for parametrization More about this image found in Input parameters for parametrization
Image
Airfoil point location definitions

Airfoil point location definitions

in Effect of Trailing Edge and Span Morphing on the Performance of an Optimized NACA6409 Wing in Ground Effect > Journal of Fluids Engineering
Published Online: September 30, 2024
Fig. 3 Airfoil point location definitions More about this image found in Airfoil point location definitions
Image
Lift and drag of fine mesh compared to experimental data at h / c ...

Lift and drag of fine mesh compared to experimental data at h / c ...

in Effect of Trailing Edge and Span Morphing on the Performance of an Optimized NACA6409 Wing in Ground Effect > Journal of Fluids Engineering
Published Online: September 30, 2024
Fig. 4 Lift and drag of fine mesh compared to experimental data at h / c  = 0.1 More about this image found in Lift and drag of fine mesh compared to experimental data at h / c ...
Image
Pareto front for each ground clearance NACA6409 wing

Pareto front for each ground clearance NACA6409 wing

in Effect of Trailing Edge and Span Morphing on the Performance of an Optimized NACA6409 Wing in Ground Effect > Journal of Fluids Engineering
Published Online: September 30, 2024
Fig. 5 Pareto front for each ground clearance NACA6409 wing More about this image found in Pareto front for each ground clearance NACA6409 wing
Image
Effect of wingtip chord on aerodynamic efficiency and aspect ratio at 4 deg...

Effect of wingtip chord on aerodynamic efficiency and aspect ratio at 4 deg...

in Effect of Trailing Edge and Span Morphing on the Performance of an Optimized NACA6409 Wing in Ground Effect > Journal of Fluids Engineering
Published Online: September 30, 2024
Fig. 6 Effect of wingtip chord on aerodynamic efficiency and aspect ratio at 4 deg root, 6 deg tip AoA, and h / c  = 0.1 More about this image found in Effect of wingtip chord on aerodynamic efficiency and aspect ratio at 4 deg...
Image
Wing sweep lower surface pressure for tip chords of 100%, 60%, 20%, and 13%...

Wing sweep lower surface pressure for tip chords of 100%, 60%, 20%, and 13%...

in Effect of Trailing Edge and Span Morphing on the Performance of an Optimized NACA6409 Wing in Ground Effect > Journal of Fluids Engineering
Published Online: September 30, 2024
Fig. 7 Wing sweep lower surface pressure for tip chords of 100%, 60%, 20%, and 13% in ground effect ( h / c  = 0.1) and 4-deg root AoA and 6-deg tip AoA More about this image found in Wing sweep lower surface pressure for tip chords of 100%, 60%, 20%, and 13%...
Image
Wingtip chord sweep for root at 4 deg root, 6 deg tip AoA, and h / c ...

Wingtip chord sweep for root at 4 deg root, 6 deg tip AoA, and h / c ...

in Effect of Trailing Edge and Span Morphing on the Performance of an Optimized NACA6409 Wing in Ground Effect > Journal of Fluids Engineering
Published Online: September 30, 2024
Fig. 8 Wingtip chord sweep for root at 4 deg root, 6 deg tip AoA, and h / c  = 0.1 More about this image found in Wingtip chord sweep for root at 4 deg root, 6 deg tip AoA, and h / c ...
Image
Streamlines of forward (top) and rear (lower) sweep wing

Streamlines of forward (top) and rear (lower) sweep wing

in Effect of Trailing Edge and Span Morphing on the Performance of an Optimized NACA6409 Wing in Ground Effect > Journal of Fluids Engineering
Published Online: September 30, 2024
Fig. 9 Streamlines of forward (top) and rear (lower) sweep wing More about this image found in Streamlines of forward (top) and rear (lower) sweep wing
Image
Optimized wing (left) with front view of wing (top right) and side (bottom ...

Optimized wing (left) with front view of wing (top right) and side (bottom ...

in Effect of Trailing Edge and Span Morphing on the Performance of an Optimized NACA6409 Wing in Ground Effect > Journal of Fluids Engineering
Published Online: September 30, 2024
Fig. 10 Optimized wing (left) with front view of wing (top right) and side (bottom right) view More about this image found in Optimized wing (left) with front view of wing (top right) and side (bottom ...
Image
Vorticity magnitude for rectangular wing ground effect ( h / c  = 0...

Vorticity magnitude for rectangular wing ground effect ( h / c  = 0...

in Effect of Trailing Edge and Span Morphing on the Performance of an Optimized NACA6409 Wing in Ground Effect > Journal of Fluids Engineering
Published Online: September 30, 2024
Fig. 11 Vorticity magnitude for rectangular wing ground effect ( h / c  = 0.1) at 0%, 10%, 20%, and 80% chord downstream More about this image found in Vorticity magnitude for rectangular wing ground effect ( h / c  = 0...