Results 21 to 30 of about 8,471 (240)

Influence of riblet shapes on the occurrence of Kelvin–Helmholtz rollers

open access: yesJournal of Fluid Mechanics, 2021
We investigate turbulent flow over streamwise-aligned riblets (grooves) of various shapes and sizes. Small riblets with spacings of typically less than $20$ viscous units are known to reduce skin-friction drag compared to a smooth wall, but larger ...
S. Endrikat   +4 more
semanticscholar   +1 more source

Effect of Riblets Geometry on Drag Reduction [PDF]

open access: yesEngineering and Technology Journal, 2010
The effect of longitudinal riblet surface models (U, V and semi-Circular and U with fillet corner riblets) on the performance of unsymmetrical airfoil (NACA23015) which has been investigated numerically and experimentally. Numerical investigation involve
Nibras M. Mahdi, Ikhlase M. Fayed
doaj   +1 more source

Drag reduction within radial turbine rotor passages using riblets [PDF]

open access: yes, 2018
In this paper, reducing the friction losses in a radial inflow turbine rotor surface by adding engineered features (riblets) is explored. Initially, computational fluid dynamics analysis was used to study the operating mechanism of riblets and to test ...
Khader, M. A., Sayma, A. I.
core   +1 more source

Drag reduction by riblets

open access: yesPhilosophical Transactions of the Royal Society A: Mathematical, Physical and Engineering Sciences, 2011
The interaction of the overlying turbulent flow with riblets, and its impact on their drag reduction properties are analysed. In the so-called viscous regime of vanishing riblet spacing, the drag reduction is proportional to the riblet size, but for larger riblets the proportionality breaks down, and the drag reduction eventually becomes ...
García Mayoral, Ricardo   +1 more
openaire   +3 more sources

Riblet-generated flow mechanisms that lead to local breaking of Reynolds analogy

open access: yesJournal of Fluid Mechanics, 2022
We investigate the Reynolds analogy over riblets, namely the analogy between the fractional increase in Stanton number $C_h$ and the fractional increase in the skin-friction coefficient $C_f$, relative to a smooth surface.
A. Rouhi   +7 more
semanticscholar   +1 more source

Direct numerical simulation of turbulent flow above zigzag riblets

open access: yesAIP Advances, 2018
We investigate the drag-reducing performance of a zigzag riblet inspired by the “Miura fold” and its influence on the streamwise vortices above a wall-bounded turbulent flow through direct numerical simulations of channel flows. The employed channel wall
Kie Okabayashi   +3 more
doaj   +1 more source

The effects of surface modification on aerodynamic characteristics of airfoil DU 06 W 200 at low Reynolds numbers,

open access: yesInternational Journal of Thermofluids, 2022
In this paper the flow characteristics and velocity fields over the vertical axis wind turbines DU 06 W 200 airfoil developed by Delft University of Technology and some other innovative designs are examined by computational fluid dynamics (CFD ...
Omid Ali Zargar   +6 more
doaj   +1 more source

Direct numerical simulation for modification of sinusoidal riblets

open access: yesJournal of Fluid Science and Technology, 2016
This paper proposes a new riblet configuration. A traditional sinusoidal riblet was modified with the aim of reducing pressure drag. The height of the side wall in the newly configured riblet is lowered toward the node of the sinusoidal curve to reduce ...
Kie OKABAYASHI
doaj   +1 more source

Turbulent structure effects due to ordered surface roughness

open access: yesAlexandria Engineering Journal, 2020
The effects of ordered surface feature in the form of converging-diverging riblets are investigated experimentally on an airfoil. Riblet sheets are applied onto the surface of NACA 0026 airfoil at a yaw angle of α=0°,±10°, Riblet height of h = 1 mm, and ...
Zambri Harun   +3 more
doaj   +1 more source

A Multisection Broadband Impedance Transforming Branch-Line Hybrid [PDF]

open access: yes, 1995
Measurements and design equations for a two section impedance transforming hybrid suitable for MMIC applications and a new method of synthesis for multisection branch-line hybrids are reported.
Danshin, T., Kumar, S., Tannous, C.
core   +2 more sources

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