Topic
Drag coefficient
About: Drag coefficient is a research topic. Over the lifetime, 14471 publications have been published within this topic receiving 303196 citations. The topic is also known as: drag factor.
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TL;DR: In this paper, it was shown how vortex-induced vibration can be practically eliminated by using free-to-rotate, two-dimensional control plates, which achieved VIV suppression with drag reduction.
189 citations
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TL;DR: In this article, a parametric computational study of energy deposition upstream of generic two-dimensional and axisymmetric blunt bodies at Mach numbers of 6.5 and 10 is performed utilizing a full Navier-Stokes computational fluid dynamics code.
Abstract: A parametric computational study of energy deposition upstream of generic two-dimensional and axisymmetric blunt bodies at Mach numbers of 6.5 and 10 is performed utilizing a full Navier-Stokes computational fluid dynamics code. The energy deposition modifies the upstream shock structure and results in large wave drag reduction and very high power effectiveness. Specifically, drag is reduced to values as low as 30% of baseline drag (no energy deposited into flow) and power effectiveness ratios (ratio of thrust power saved to power deposited into the flow) of up to 33 are obtained. The fluid dynamic and thermodynamic bases of the observed drag reduction are examined
189 citations
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TL;DR: In this paper, it was shown that the boundary layer approximation to the flow of a viscous fluid past a flat plate of length l, generally valid near the plate when the Reynolds number Re is large, fails within a distance O(lRe$^{-\frac{3}{4}}$) of the trailing edge.
Abstract: It is shown that the boundary layer approximation to the flow of a viscous fluid past a flat plate of length l, generally valid near the plate when the Reynolds number Re is large, fails within a distance O(lRe$^{-\frac{3}{4}}$) of the trailing edge. The appropriate governing equations in this neighbourhood are the full Navier-Stokes equations. On the basis of Imai (1966) these equations are linearized with respect to a uniform shear and are then completely solved by means of a Wiener-Hopf integral equation. The solution so obtained joins smoothly on to that of the boundary layer for a flat plate upstream of the trailing edge and for a wake down-stream of the trailing edge. The contribution to the drag coefficient is found to be O(Re$^{-\frac{3}{4}}$) and the multiplicative constant is explicitly worked out for the linearized equations.
188 citations
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TL;DR: A family of wing motion parameterized by the inclined angle of the stroke plane is studied, which suggests a strategy for improving efficiency of normal hovering, and a unifying view of different wing motions employed by insects.
Abstract: SUMMARY Studies of insect flight have focused on aerodynamic lift, both in
quasi-steady and unsteady regimes. This is partly influenced by the choice of
hovering motions along a horizontal stroke plane, where aerodynamic drag makes
no contribution to the vertical force. In contrast, some of the best hoverers–
dragonflies and hoverflies – employ inclined stroke planes,
where the drag in the down- and upstrokes does not cancel each other. Here,
computation of an idealized dragonfly wing motion shows that a dragonfly uses
drag to support about three quarters of its weight. This can explain an
anomalous factor of four in previous estimates of dragonfly lift coefficients,
where drag was assumed to be small. To investigate force generation and energy cost of hovering flight using
different combination of lift and drag, I study a family of wing motion
parameterized by the inclined angle of the stroke plane. The lift-to-drag
ratio is no longer a measure of efficiency, except in the case of horizontal
stroke plane. In addition, because the flow is highly stalled, lift and drag
are of comparable magnitude, and the aerodynamic efficiency is roughly the
same up to an inclined angle about 60°, which curiously agrees with the
angle observed in dragonfly flight. Finally, the lessons from this special family of wing motion suggests a
strategy for improving efficiency of normal hovering, and a unifying view of
different wing motions employed by insects.
188 citations
01 Feb 1924
TL;DR: The most important part of the resistance or drag of a wing system, the induced drag, can be calculated theoretically, when the distribution of lift on the individual wings is known as mentioned in this paper.
Abstract: The most important part of the resistance or drag of a wing system,the induced drag, can be calculated theoretically, when the distribution of lift on the individual wings is known. The calculation is based upon the assumption that the lift on the wings is distributed along the wing in proportion to the ordinates of a semi-ellipse. Formulas and numerical tables are given for calculating the drag. In this connection, the most favorable arrangements of biplanes and triplanes are discussed and the results are further elucidated by means of numerical examples.
188 citations