Results 151 to 160 of about 92,283 (210)
Gyroid as a novel approach to suppress vortex shedding and mitigate induced vibration. [PDF]
Berger T, Farhat M.
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The interaction of 2D vortices in a developing pulsed plasma jet. [PDF]
Dong L, Choi KS, Wang Y.
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Fish Scale-Inspired Flow Control for Corner Vortex Suppression in Compressor Cascades. [PDF]
Shen JL, Yang HC, Yeh SI.
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A topological hypothesis for atrial fibrilllation, atrial flutter and focal atrial tachycardia: comparison and contrast with Kosterlitz-Thouless physics. [PDF]
Ganesan AN, Kuklik P, Nattel S.
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Numerical investigation of low-frequency shock train oscillations in a divergent isolator with vortex generator jets. [PDF]
Wang J, He K, Zhou Q, Wang J.
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Impact of Biomimetic Fin on Pitching Characteristics of a Hydrofoil. [PDF]
Ikram F +8 more
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Leading-Edge Vortex Lifts Swifts
Science, 2004The current understanding of how birds fly must be revised, because birds use their hand-wings in an unconventional way to generate lift and drag. Physical models of a common swift wing in gliding posture with a 60° sweep of the sharp hand-wing leading edge were tested in a water tunnel.
Videler, J. J. +2 more
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Vortex–leading-edge interaction
Journal of Fluid Mechanics, 1982Visualization of successive vortices impinging upon the leading edge of a wedge reveals patterns of deformation of each incident vortex; for certain offsets of the edge with respect to the incident vortex there is pronounced vortex shedding from the leading edge, whereby the shed vortex has a vorticity orientation opposite to that of the incident ...
Samir Ziada, Donald Rockwell
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Lift and the Leading Edge Vortex
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 2012AbstractFlapping wings often feature a leading-edge vortex (LEV) that is thought to enhance the lift generated by the wing. Here the lift on a wing featuring a leading-edge vortex is considered by performing experiments on a translating flat-plate aerofoil that is accelerated from rest in a water towing tank at a fixed angle of attack of 15°.
Pitt Ford, C. W., Babinsky, H.
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