共 5 条
Effects of surface roughness on the drag coefficient of finite-span cylinders freely rolling on an inclined plane
被引:0
|作者:
Nanayakkara, S. D. J. S.
[1
]
Zhao, J.
[1
,2
]
Terrington, S. J.
[1
]
Thompson, M. C.
[1
]
Hourigan, K.
[1
]
机构:
[1] Monash Univ, Dept Mech & Aerosp Engn, FLAIR, Clayton, Vic 3800, Australia
[2] Univ New South Wales, Sch Engn & Technol, Canberra, ACT 2610, Australia
基金:
澳大利亚研究理事会;
关键词:
sediment transport;
lubrication theory;
vortex shedding;
CIRCULAR-CYLINDER;
NONCOLLOIDAL SPHERE;
REYNOLDS-NUMBER;
SLOW MOTION;
FLOW;
WAKE;
WALL;
DYNAMICS;
PARALLEL;
ROTATION;
D O I:
10.1017/jfm.2024.833
中图分类号:
O3 [力学];
学科分类号:
08 ;
0801 ;
摘要:
We present an experimental investigation aimed at understanding the effects of surface roughness on the time-mean drag coefficient ((C) over bar (D)) of finite-span cylinders (span/diameter = aspect ratio, 0.51 <= AR <= 6.02) freely rolling without slip on an inclined plane. While lubrication theory predicts an infinite drag force for ideally smooth cylinders in contact with a smooth surface, experiments yield finite drag coefficients. We propose that surface roughness introduces an effective gap (G(eff)) resulting in a finite drag force while allowing physical contact between the cylinder and the plane. This study combines measurements of surface roughness for both the cylinder and the plane panel to determine a total relative roughness (xi) that can effectively describe G(eff) at the point of contact. It is observed that the measured (C) over bar (D) increases as xi decreases, aligning with predictions of lubrication theory. Furthermore, the measured (C) over bar (D) approximately matches combined analytical and numerical predictions for a smooth cylinder and plane when the imposed gap is approximately equal to the mean peak roughness (R-p) for rough cylinders, and one standard deviation peak roughness (R-p,R-1 sigma) for relatively smooth cylinders. As the time-mean Reynolds number ((Re) over bar) increases, the influence of surface roughness on (C) over bar (D) decreases, indicating that wake drag becomes dominant at higher (Re) over bar. The cylinder aspect ratio (AR) is found to have little impact on (C) over bar (D). Flow visualisations are also conducted to identify critical flow transitions and these are compared with visualisations previously obtained numerically. Variations in xi have little effect on the cylinder wake. Instead, AR was observed to have a more pronounced impact on the flow structures observed. The Strouhal number (St) associated with the cylinder wake shedding was observed to increase with (Re) over bar, while demonstrating little dependence on AR.
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