Aerodynamic Instability Mechanisms of Iced Eight-Bundled Conductors: Frequency-Domain Analysis and Stability Assessment via Wind Tunnel-CFD Synergy. [PDF]
Zhong B, Qiao M, Cai M, Hu M.
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Unlocking Microbial Dark Matter: A Comprehensive Review of Isolation Technologies from Traditional Culturing to Single-Cell Technologies. [PDF]
Sun X, Zhang X, Zhang J.
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Enhancing start-up and torque in Darrieus VAWTs through a novel plain gurney flap design. [PDF]
Eltayeb W +4 more
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Study of sand particle motion characteristics and distribution patterns in a helical-blade multiphase pump. [PDF]
Zhao X, Shi G, Cui Z, Zhang Y.
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Large dynamic pitching for lift enhancement during the pull-out manoeuvre of raptors. [PDF]
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Connection between leading-edge sweep, vortex lift, and vortex strength for delta wings
Journal of Aircraft, 1990An effort is made to clarify the effect of leading-edge sweep on the vortex lift and leading-edge vortex strength of a slender wing; while it is often assumed that increasing sweep enhances vortex lift and strength, the opposite is the case. The suction analogy is used in association with numerical and experimental data to derive simple formulas ...
Michael J. Hemsch, James M. Luckring
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Remarks on Nonlinear Lift and Vortex Separation
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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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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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