Effect of attack angle fluctuation superimposed on the cross-flow oscillation of a rectangular cylinder in uniform flow

2002 ◽  
Vol 2002.7 (0) ◽  
pp. 131-132
Author(s):  
Yuuki KUBO ◽  
Mizuyasu KOIDE ◽  
Tsutomu TAKAHASHI ◽  
Masataka SHIRAKASHI
Author(s):  
Mizuyasu Koide ◽  
Tsutomu Takahashi ◽  
Masataka Shirakashi ◽  
Yuuki Kubo ◽  
La´szlo´ Baranyi

The cross-flow oscillation of a rectangular cylinder supported by a cantilever plate-spring system was investigated using a wind tunnel, in order to reveal the effect of attack angle fluctuation superimposed on cross-flow oscillation. Three kinds of support systems were tested in order to give a different phase-shift between attack angle and cylinder displacement. Three rectangular cylinders with the slenderness of 0.5, 1.0 and 2.0 were used to investigate effect of attack angle both on the Ka´rma´n vortex excitation and the galloping. The effect of attack angle fluctuation on oscillation behavior markedly differed among the three rectangular cylinders of different slenderness. When the slenderness was 0.5, attack angle fluctuation had no influence on the oscillation behavior of the cylinder. When the slenderness was 1.0 and 2.0, the oscillation behavior was quite different compared with pure cross-flow oscillation, depending on the support system and slenderness.


2009 ◽  
Vol 2009.46 (0) ◽  
pp. 509-510
Author(s):  
Takeshi HAGINOYA ◽  
Yusuke KAWABATA ◽  
Mizuyasu KOIDE ◽  
Tsutomu TAKAHASHI ◽  
Masataka SHIRAKASHI

1972 ◽  
Vol 23 (4) ◽  
pp. 263-275 ◽  
Author(s):  
W H Hui

SummaryA unified theory is given of hypersonic and supersonic flow over the lower surface of a caret wing at certain off-design conditions when the bow shock is attached to the leading edges of the wing and when there exists no internal shock. The flow field on the lower surface of a caret wing consists of uniform flow regions near the leading edges, where the cross-flow is supersonic, and a non-uniform flow in the central region, where the cross-flow is subsonic. The basic assumption is that the flow in the central region differs slightly from the two-dimensional supersonic flow over a flat plate at the same angle of incidence as that of the lower ridge of the wing. Based on this assumption, a first-order perturbation flow is first calculated and then strained and corrected so that it matches the uniform flow which is obtained exactly. Slope discontinuities of the pressure curve are found at the cross-flow sonic line. Numerical examples and comparisons with previous theories and experiments are included.


Author(s):  
Atsushi Enya ◽  
Atsushi Okajima

It is important for industrial purposes to predict flow-induced vibration of a bluff body elastically supported in an uniform flow. In this paper, the free oscillation of a rectangular cylinder with two-degree of freedom in the streamwise (in-line) and cross-flow (transverse) directions in a uniform flow, was computed by the Large Eddy Simulation (LES) method at high Reynolds number of 2.2 × 104. The Smagorinsky model was used as a subgrid scale (SGS) model. The main objectives of this work were to predict and estimate characteristics of flows around a free-oscillating cylinder. The present computations successfully reproduce various types of flow-induced vibrations of a free-oscillating rectangular cylinder as found by experiments; in-line oscillation, eddy-excitation and low-velocity galloping.


Author(s):  
Richard J. McSherry ◽  
Richard H. J. Willden ◽  
J. Michael R. Graham

Presented in this paper is a comparison between numerical and experimental investigations of the Vortex-Induced Vibrations of a model scale marine riser pipe, length-to-diameter ratio of approximately 1400, that was subjected to sub-critical Reynolds number flows. The experiments, which were commissioned by the Norweigan Deepwater Programme, were carried out at Marintek’s Ocean Basin in Trondheim in 2003. The numerical simulations are performed using a coupled Computational Fluid-Structural dynamics code. The fluid flow is computed using Large Eddy Simulation, on multiple two-dimensional strips that are positioned at intervals along the length of the riser. The numerical riser response predictions are found to agree well with the experimental measurements. Of particular note was the occurrence in the simulations of harmonic responses at multiples of the principal oscillation frequency; in the cross-flow direction at three and five times the cross-flow oscillation frequency, and in the in-line direction at two and three times the in-line oscillation frequency. Also presented in the paper are the results of a rigorous benchmarking of the code’s two-dimensional flow solver against high-quality data from forced cross-flow oscillation experiments performed at sub-critical Reynolds numbers; the code predicted the lift force and phase angle variations well, although agreement in the mean drag force variation was less good.


2004 ◽  
Vol 126 (5) ◽  
pp. 884-887 ◽  
Author(s):  
Mizuyasu Koide ◽  
Yuuki Kubo ◽  
Tsutomu Takahashi ◽  
La´szlo´ Baranyi ◽  
Masataka Shirakashi

2001 ◽  
Vol 1 (5-6) ◽  
pp. 39-47
Author(s):  
Y. Matsui ◽  
A. Yuasa ◽  
F. Colas

The effects of operational modes on the removal of a synthetic organic chemical (SOC) in natural water by powdered activated carbon (PAC) during ultrafiltration (UF) were studied, through model simulations and experiments. The removal percentage of the trace SOC was independent of its influent concentration for a given PAC dose. The minimum PAC dosage required to achieve a desired effluent concentration could quickly be optimized from the C/C0 plot as a function of the PAC dosage. The cross-flow operation was not advantageous over the dead-end regarding the SOC removal. Added PAC was re-circulated as a suspension in the UF loop for only a short time even under the cross-flow velocity of gt; 1.0 m/s. The cross-flow condition did not contribute much to the suspending of PAC. The pulse PAC addition at the beginning of a filtration cycle resulted in somewhat better SOC removal than the continuous PAC addition. The increased NOM loading on PAC which was dosed in a pulse and stayed longer in the UF loop could possibly further decrease the adsorption rate.


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