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1.
The flow field around a rotationally oscillating circular cylinder in a uniform flow is studied by using a particle image
velocimetry to understand the mechanism of drag reduction and the corresponding suppression of vortex shedding in the cylinder
wake at low Reynolds number. Experiments are conducted on the flow around the circular cylinder under rotational oscillation
at forcing Strouhal number 1, rotational amplitude 2 and Reynolds number 2,000. It is found from the flow measurement by PIV
that the width of the wake is narrowed and the velocity fluctuations are reduced by the rotational oscillation of the cylinder,
which results in the drag reduction rate of 30%. The mechanism of drag reduction is studied by phase-averaged PIV measurement,
which indicates the formation of periodic small-scale vortices from both sides of the cylinder. It is found from the cross-correlation
measurement between the velocity fluctuations that the large-scale structure of vortex shedding is almost removed in the cylinder
wake, when the small-scale vortices are generated at the unstable frequency of shear layer by the influence of rotational
oscillation. 相似文献
2.
Computer experiments were performed to explore the flow in the vicinity of a truncated normal flat plate in a rapidly rotating fluid. A Taylor column formed above the flat plate and the vortex shedding in the wake of the Taylor column closely resembled the vortex street behind the solid plate. This is probably the first observation of a Kármán vortex street behind a Taylor column in a computational study. 相似文献
3.
Flow past a square prism with cut-corners at the front-edge is numerically and experimentally visualized to investigate a
mechanism of drag reduction. An adaptive numerical scheme based on the vortex method is implemented for two values of the
Reynolds number between 200 and 1,250, and the results are compared with experiments. Experimental visualization techniques
include the hydrogen-bubble technique atRe=4,000 and the oil-flow technique atRe=10,000 for a global wake formation, and the aluminum-flake technique for transient flow at the early stage of motion atRe=1,250. A similar reattachment flow pattern is shown in a wide range of the Reynolds number between 200 and 10,000, which
implies a possibility of the drag reduction in the Reynolds number being approximately lower than 8,000 unlike the previous
findings. 相似文献
4.
V. I. Kornilov 《Thermophysics and Aeromechanics》2010,17(2):249-258
Experiments are performed to study the possibility of decreasing the net drag of a flat plate with the use of streamwise-oriented
vertical elements mounted normal to the surface in an incompressible equilibrium turbulent boundary layer. The Reynolds number
based on the boundary-layer momentum thickness in the section where the vertical elements are placed is 820. It is demonstrated
that vertical large eddy breakup elements with the geometry used do not reduce the drag of a flat plate in the major part
of the range of Reynolds numbers Re
x
examined. It is only at extremely low values of Re
x
that a certain gain in the net drag is reached, as compared with the value for a non-modified flow. 相似文献
5.
6.
Abstract
It is known that for a square cylinder subjected to uniform flow, the drag force changes with the angle of attack. To clarify the flow characteristics around a square cylinder with corner cutoffs, we measured the drag coefficient and the Strouhal number for changing chamfer dimensions. We analyzed the flow around a square cylinder with corner cutoffs by applying the RNG k–ε turbulent model, and investigated the surface flow pattern using visualization by means of the oil film and mist flow method. From these results, we obtained the surface flow patterns by the oil film method and numerical analysis. The numerical results agreed well with the experimental values. The drag coefficient of the square cylinder with corner cutoffs decreased suddenly at an angle of attack of about α = 0°– 10° when compared with the drag coefficient for a square cylinder. The minimum value of the drag coefficient for the square cylinder with corner cutoffs decreased by about 30% compared with that for the square cylinder. The drag coefficient of the square cylinder with 10% corner cutoffs was found to be smallest, since the wake area of this square cylinder was smaller compared with that of the other square cylinder. 相似文献7.
The possibility of decreasing the turbulent friction with the use of streamwise-aligned vertical large eddy breakup devices
installed normal to the surface of a flat plate in an incompressible equilibrium turbulent boundary layer with a nominally
gradientless flow past this plate is studied experimentally. The Reynolds number based on the boundary-layer momentum thickness
is 1099 in the cross section where these vertical devices are mounted. It is shown that elements of this geometry are effective
tools for modification of the turbulent boundary layer from the viewpoint of both the gain in friction drag and the suppression
of turbulent fluctuations of velocity and, hence, can be considered as one of the most important factors of controlling the
structure of the near-wall turbulence in the flow past a flat surface. 相似文献
8.
The near wake of a varicose cylinder has been experimentally investigated using Laser Induced Fluorescence (LIF) and Digital
Particle Imaging Velocimetry (DPIV). The work aims to provide understanding to the mechanism of the cross flow around varicose
cylinder as well as to comprehend why the introduction of relatively small degrees of spanwise waviness can have a significant
effect on drag reduction and suppression of the cylinder vibration. The evolution of the flow patterns and the corresponding
vortex interactions are obtained. The experimental results indicated that the wake width and the formation length vary along
the span of the varicose cylinder. A wider wake and a longer formation length were observed in the saddle plane. In addition,
an interpretation of the three-dimensional wake structures is postulated and conceptually shown. The numerical simulation
by 3-D finite volume method is successful in predicting the flow features found by the experiments. 相似文献
9.
10.
本文在涡团法的基础上结合有限元法及无限相似单元法在整个无界的流动区域上构造了Navier-Stokes方程的数值解,成功地克服了区域边界上凸角点邻域内解的奇性给数值计算带来的困难,同时克服了无穷远点给数值计算带来的困难。本文对平板大攻角平面绕流问题进行数值模拟,给出了初步的计算结果。 相似文献
11.
The interaction of resonant sounds with the flow past a thick, blunt, flat plate in a rigid walled square duct has been examined. Sound pressure levels of up to 146 dB (re 20 μPa) have been recorded. It has been established that the resonant sound can initially be excited at a harmonic of the normal vortex shedding frequency. In some cases, the sound “feeds back” on the vortex shedding process causing a step change in the shedding frequency, increasing the Strouhal number for the plate by up to twice the normal value. This excited vortex shedding and associated resonances can be suppressed by locating the plate at incidence to the air flow direction. Complex duct modes can be generated by the vortex shedding resulting in different regions of the plate shedding at different Strouhal numbers. 相似文献
12.
The influence of Reynolds number and blockage ratio on the vortex dynamics of a trapezoidal bluff body placed inside a circular pipe is studied experimentally and numerically. Low aspect ratio, high blockage ratio, curved end conditions (junction of pipe and bluff body), axisymmetric upstream flow with shear and turbulence are some of the intrinsic features of this class of bluff body flows which have been scarcely addressed in the literature. A large range (200:200,000) of Reynolds number (ReD) is covered in this study, encompassing all the three pipe flow regimes (laminar, transition and turbulent). Four different flow regimes are defined based on the distinct features of Strouhal number (St)–ReD relation: steady, laminar irregular, transition and turbulent. The wake in the steady regime is stationary with no oscillations in the shear layer. The laminar regime is termed as irregular owing to irregular vortex shedding. The vortex shedding in this regime is observed to be symmetric. The emergence of separation bubble downstream of the bluff body on either side is another interesting feature of this regime, which is further observed to be symmetric. Two pairs of mean streamwise vortices are noticed in the near-wake regime, which are termed as reverse dipole-type wake topology. Beyond the irregular laminar regime, the Strouhal number falls gradually and vortex shedding becomes more periodic. This regime is named transition and occurs close to the Reynolds number at which transition to turbulence takes place in a fully developed pipe. The turbulent regime is characterised by a nearly constant Strouhal number. Typical Karman-type vortex shedding is noticed in this regime. The convection velocity, wake width formation length and irrecoverable pressure loss are quantified to highlight the influence of blockage ratio. These results will be useful to develop basic understanding of vortex dynamics of confined bluff body flow for several practical applications. 相似文献
13.
The wake of a streamwise oscillating cylinder is presently investigated. The Reynolds number investigated is 300, based on
the cylinder diameterd. The cylinder oscillates at an amplitude of 0.5d and a frequencyf
e/fs=1.8, wheref
e is the cylinder oscillating frequency andf
s is the natural vortex shedding frequency of a stationary cylinder. Under these conditions the flow is essentially two dimensional.
A two-dimensional direct numerical simulation (DNS) scheme has been developed to calculate the flow. The DNS results display
a street of binary vortices, each containing two counter-rotating vortical structures, symmetrical about the centerline, which
is in excellent agreement with measurements. The drag and lift on the cylinder have been examined. The time averaged drag
and lift are 1.4 and 0, respectively, which are the same as those on a stationary cylinder at the sameRe. However, the fluctuating drag was high, about 2.68. It has been found that, being symmetrically formed about the centerline,
the binary vortices induce an essentially zero fluctuating lift, which may have a profound implication in flow control and
engineering. 相似文献
14.
《Revue Generale de Thermique》1997,36(1):17-25
This study deals with aerodynamics phenomena in a rapid compression machine. The mixture is initially at rest in the cylinder, and the piston is at bottom dead center; therefore there is no flow generated during the intake stroke. Moreover, flat and parallel piston and cylinder-head faces avoid squish flow. A corner vortex is generated when the piston surface, moving toward the top dead center, scrapes the boundary layer on the cylinder wall. This vortex is visualized by shadowgraph and then modeled to evaluate its characteristics. During the expansion, the gas trapped in the crevices between the piston, piston ring and cylinder wall flows back into the combustion chamber. Both crevice jet and corner vortex exist in real engines and their interactions with combustion are important: the corner vortex impairs flame kernel development and the crevice gases constitute a major source of unburnt gas. 相似文献
15.
In this paper, hot-wire anemometry (HWA) is used to experimentally investigate interactions between a fully developed turbulent boundary layer and wake of an elliptic cylinder where axis ratio (AR) of the cylinder is 2. The elliptic cylinder was located inside and outside a turbulent boundary layer with a thickness (δ) of 0.38B. Furthermore, experiments were conducted at different Reynolds numbers (13,250 and 26,500) based upon the smallest cylinder diameter (B). Mean velocity, turbulence intensity and higher-order central moments of velocity signals (i.e. skewness and flatness) measurements were performed using HWA upon wake-boundary layer interactions on a flat plate. Results showed that profiles of stream-wise mean velocity and turbulence intensity were greatly dependent on gap ratio (G/B) and Reynolds number (Re) in near-wake region. It was also observed that, except for G/B = 0.1, the wake-boundary layer interactions were faster at Reynolds number of 26,500 rather than 13,250. The interactions occurred earlier upon fluctuating the velocity rather than the case where a fixed mean velocity was considered. The results further show that an increase in the gap ratio increases Strouhal number almost independent of δ/B. Behind the cylinder, relatively smaller wake region was obtained at Re = 26,500 rather than Re = 13,250, where the velocity profiles quickly converged to the flat plate boundary layer velocity profiles. 相似文献
16.
Experimental Study on Physical Mechanism of Drag Reduction of Hydrophobic Materials in Laminar Flow
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We experimentally study the physical mechanism of the drag reduction of hydrophobic materials in the macroscopic scale. The experiment includes the drag and velocity measurements of laminar boundary layer flow over flat plates, and the observation of air bubbles on the surfaces. The plate surfaces have different wetting and roughness properties. In the drag measurements, the plates with bubbles on the surfaces lead to drag reduction, but not for those without bubbles. Velocity measurement confirms that the flow is laminar and gives apparent fluid slip on the plate wall with bubbles. In observation, air bubbles in macroscopic size emerge and enlarge on hydrophobic surfaces but not on hydrophilic surfaces. Therefore, the drag reduction of hydrophobic materials is explained by the generation of air bubbles of macroscopic size that cause the apparent velocity slip. 相似文献
17.
The fully 3D turbulent incompressible flow around a cylinder and in its wake at a Reynolds number Re = = 9×104 based on the cylinder diameter and Mach number M = 0.1 is calculated using Large Eddy Simulations (LES). Encouraging results are found in comparison to experimental data for the fluctuating lift and drag forces. The acoustic pressure in far-field is commutated through the surface integral formulation of the Ffowcs Williams and Hawkings (FWH) equation in acoustic analogy. Five different sound sources, the cylinder wall and four permeable surfaces in the flow fields, are employed. The spectra of the sound pressure are generally in quantitative agreement with the measured one though the acoustic sources are pseudo-sound regarding the incompressible flow simulation. The acoustic component at the Strouhal number related to vortex shedding has been predicted accurately. For the broad band sound, the permeable surfaces in the near wake region give qualitative enough accuracy level of predictions, while the cylinder wall surface shows a noticeable under-prediction. The sound radiation of the volumetric sources based on Lighthill tensors at vortex shedding is also studied. Its far-field directivity is of lateral quadrupoles with the weak radiations in the flow and cross-flow directions. 相似文献
18.
建立多孔结构覆面柱体绕流模型, 采用含Darcy-Brinkman-Forchheimer作用力项的格子Boltzmann方程对覆盖多孔介质层的方柱绕流进行数值模拟, 研究多孔介质对钝体绕流流场特性的影响。结果表明: 相比于不可渗透壁的柱体, 引入合适参数的多孔介质覆面层后可以有效降低其升力脉动幅值, 但阻力有所增加。同时, 较高雷诺数下多孔方柱的数值模拟表明: 多孔介质壁面使得尾迹区域的剪切层相距更远, 降低了尾流处湍动能, 并将雷诺应力的峰值移动到尾迹区域, 抑制了方柱两侧的动量交换, 使动量交换的位置发生在尾迹区域, 继而使得尾迹的涡街更加规则化。 相似文献
19.
We measure, using a lattice gas algorithm, the time development of a wake behind a cylinder at Reynolds numbers equal to 30 and 60. We measure also drag at these values and determine Re90 to be the Reynolds number where vortex shedding starts. Agreement with experimental results is good. We also measure vortex shedding frequency at Re = 108 from transverse velocity and at Re = 180 from lift on the cylinder. The corresponding Strouhal numbers are obtained and discussed. 相似文献