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Numerical studies on the dynamics of an open triangle in a vertically oscillatory flow

Published online by Cambridge University Press:  05 January 2016

Xueming Shao
Affiliation:
State Key Laboratory of Fluid Power Transmission and Control, Department of Mechanics, Zhejiang University, Hangzhou 310027, China
Xiaolong Zhang
Affiliation:
State Key Laboratory of Fluid Power Transmission and Control, Department of Mechanics, Zhejiang University, Hangzhou 310027, China
Zhaosheng Yu*
Affiliation:
State Key Laboratory of Fluid Power Transmission and Control, Department of Mechanics, Zhejiang University, Hangzhou 310027, China
Jianzhong Lin
Affiliation:
State Key Laboratory of Fluid Power Transmission and Control, Department of Mechanics, Zhejiang University, Hangzhou 310027, China
*
Email address for correspondence: [email protected]

Abstract

A direct-forcing fictitious domain method is employed to study the dynamics of an open triangle in a vertically oscillatory flow. The flow structures, the vertical force and the torque on the fixed body are analysed for the stable flow regime in which the flow structures form and evolve exactly in the same way in each period and the unstable regime, respectively. Our results indicate that in the stable flow regime for the body with upright orientation, the steady streaming structure mainly comprises two vortex pairs located respectively above and below the body. Due to up–down asymmetry of the body, the pair below the body produces a larger vertical force on the body than the upper pair, which is mainly responsible for the non-zero average force at relatively high Reynolds numbers. The average force increases with increasing Reynolds number or increasing dimensionless period for the parameter range studied, due to the vortex effects. In the unstable regime, a vortex pair is ejected downward from each body edge. The irregular motion of the emitted vortices below the body leads to the irregular fluctuation of the vertical force. Regarding the torque on a tilted body, in the stable regime, the body experiences a restoring torque when its vertex angle is larger than a critical value being close to (and smaller than) 60°, and otherwise a destructive torque, irrespective of the value of tilt angle. For a fixed vertex angle, the torque magnitude is largest when the tilt angle is around 45°. In the unstable regime, the persistent ejection of the vortex pair during upward flow and corresponding restoring torque are observed for a large tilt angle with one edge aligned close to the horizontal direction, as in the experiment of Liu et al. (Phys. Rev. Lett., vol. 108, 2012, 068103). For a relatively small tilt angle, the emission direction of the vortex pair has intermittency, leading to the intermittency in the direction of torque. The reasons for the above observations are discussed. The predictions on the stable orientation for a hovering body in the stable flow regime and the irregular orientation in the unstable regime are confirmed in the dynamic simulation of a freely moving body. The body with the stable horizontal orientation in case of small vertex angle migrates along the body-shape-diverging direction.

Type
Papers
Copyright
© 2016 Cambridge University Press 

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References

An, H., Cheng, L. & Zhao, M. 2009 Steady streaming around a circular cylinder in an oscillatory flow. Ocean Engng 36, 10891097.Google Scholar
An, H., Cheng, L. & Zhao, M. 2011a Direct numerical simulation of oscillatory flow around a circular cylinder at low Keulegan–Carpenter number. J. Fluid Mech. 666, 77103.Google Scholar
An, H., Cheng, L. & Zhao, M. 2011b Steady streaming around a circular cylinder near a plane boundary due to oscillatory flow. J. Hydraul. Engng ASCE 137, 2333.CrossRefGoogle Scholar
Anagnostopoulos, P. & Dikarou, C. 2011 Numerical simulation of viscous oscillatory flow past four cylinders in square arrangement. J. Fluids Struct. 27, 212232.Google Scholar
Azuma, A. 2006 The Biokinetics of Flying and Swimming, 2nd edn. AIAA Education.CrossRefGoogle Scholar
Bearman, P. W., Graham, J. M. R., Obasaju, E. D. & Drossopulos, G. M. 1984 The influence of corner radius on the forces experienced by cylindrical bluff bodies in oscillatory flow. Appl. Ocean Res. 6, 8389.CrossRefGoogle Scholar
Chern, M. J., Kanna, P. R., Lu, Y. J., Cheng, I. C. & Chang, S. C. 2010 A CFD study of the interaction of oscillatory flows with a pair of side-by-side cylinders. J. Fluids Struct. 26, 626643.CrossRefGoogle Scholar
Chern, M. J., Shiu, W. C. & Horng, T. L. 2013 Immersed boundary modeling for interaction of oscillatory flow with cylinder array under effects of flow direction and cylinder arrangement. J. Fluids Struct. 43, 325346.CrossRefGoogle Scholar
Childress, S., Vandenberghe, N. & Zhang, J. 2006 Hovering of a passive body in an oscillating airflow. Phys. Fluids 18, 117103.CrossRefGoogle Scholar
Coenen, W. 2013 Oscillatory flow about a cylinder pair with unequal radii. Fluid Dyn. Res. 45, 055511.CrossRefGoogle Scholar
Glowinski, R., Pan, T. W., Hesla, T. I. & Joseph, D. D. 1999 A distributed Lagrange multiplier/fictitious domain method for particulate flows. Intl J. Multiphase Flow 25, 755794.Google Scholar
Holtsmark, J., Johnsen, I., Sikkeland, T. & Skavlem, S. 1954 Boundary layer flow near a cylindrical obstacle in an oscillating incompressible fluid. J. Acoust. Soc. Am. 26, 2639.Google Scholar
Iliadis, G. & Anagnostopoulos, P. 1998 Viscous oscillatory flow around a circular cylinder at low Keulegan–Carpenter numbers and frequency parameters. Intl J. Numer. Meth. Fluids 26, 403442.3.0.CO;2-V>CrossRefGoogle Scholar
Joseph, D. D. & Liu, Y. J. 1993 Orientation of long bodies falling in a viscoelastic liquid. J. Rheol. 37, 961983.Google Scholar
Klotsa, D., Swift, M. R., Bowley, R. M. & King, P. J. 2009 Chain formation of spheres in oscillatory fluid flows. Phys. Rev. E 79, 021302.Google Scholar
Lehmann, F. O. 2004 The mechanisms of lift enhancement in insect flight. Naturwissenschaften 91, 101122.Google Scholar
Liu, B., Ristroph, L., Weathers, A., Childress, S. & Zhang, J. 2012 Intrinsic stability of a body hovering in an oscillating airflow. Phys. Rev. Lett. 108, 068103.Google Scholar
Lu, X., Dalton, C. & Zhang, J. 1997 Application of large eddy simulation to an oscillating flow past a circular cylinder. Trans. ASME J. Fluids Engng 119, 519525.Google Scholar
Pacheco-Martinez, H. A., Liao, L., Hill, R. J. A., Swift, M. R. & Bowley, R. M. 2013 Spontaneous orbiting of two spheres levitated in a vibrated liquid. Phys. Rev. Lett. 110, 154501.Google Scholar
Rednikov, A. Y. & Sadhal, S. S. 2004 Steady streaming from an oblate spheroid due to vibrations along its axis. J. Fluid Mech. 499, 345380.CrossRefGoogle Scholar
Riley, N. 1966 On a sphere oscillating in a viscous fluid. Q. J. Mech. Appl. Maths 19, 461472.CrossRefGoogle Scholar
Riley, N. 2001 Steady streaming. Annu. Rev. Fluid Mech. 33, 4365.Google Scholar
Sane, S. P. 2003 The aerodynamics of insect flight. J. Expl Biol. 206, 41914208.CrossRefGoogle ScholarPubMed
Sarpkaya, T. 1986 Forces on a circular cylinder in viscous oscillatory flow at low Keulegan–Carpenter numbers. J. Fluid Mech. 165, 6171.Google Scholar
Spagnolie, S. E. & Shelley, M. J. 2009. Shape-changing bodies in fluid: hovering, ratcheting, and bursting. Phys. Fluids 21, 013103.Google Scholar
Stuart, J. T. 1966 Double boundary layer in oscillatory viscous flow. J. Fluid Mech. 24, 673687.Google Scholar
Van Dyke, M. 1982 An Album of Fluid Motion. Parabolic.Google Scholar
Wang, C. Y. 1968 On high-frequency oscillatory viscous flows. J. Fluid Mech. 32, 5568.Google Scholar
Wang, Z. J. 2005 Dissecting insect flight. Annu. Rev. Fluid Mech. 37, 183210.CrossRefGoogle Scholar
Weathers, A., Folie, B., Liu, B., Childress, S. & Zhang, J. 2010 Hovering of a rigid pyramid in an oscillatory airflow. J. Fluid Mech. 650, 415425.CrossRefGoogle Scholar
Williamson, C. H. K. 1985 Sinusoidal flow relative to circular cylinders. J. Fluid Mech. 155, 141174.Google Scholar
Wright, H. S., Swift, M. R. & King, P. J. 2008 Migration of an asymmetric dimer in oscillatory fluid flow. Phys. Rev. E 78, 036311.Google Scholar
Wunenburger, R., Carrier, V. & Garrabos, Y. 2002 Periodic order induced by horizontal vibrations in a two-dimensional assembly of heavy beads in water. Phys. Fluids 14, 23502359.CrossRefGoogle Scholar
Yu, Z. S. & Shao, X. M. 2007 A direct-forcing fictitious domain method for particulate flows. J. Comput. Phys. 227, 292314.Google Scholar
Yu, Z., Shao, X. & Wachs, A. 2006a A fictitious domain method for particulate flows with heat transfer. J. Comput. Phys. 217, 424452.CrossRefGoogle Scholar
Yu, Z., Wachs, A. & Peysson, Y. 2006b Numerical simulation of particle sedimentation in shear-thinning fluids with a fictitious domain method. J. Non-Newtonian Fluid Mech. 136, 126139.Google Scholar
Zhao, H., Sadhal, S. S. & Trinh, E. H. 1999 Singular perturbation analysis of an acoustically levitated sphere: flow about the velocity node. J. Acoust. Soc. Am. 106, 589595.Google Scholar
Zheng, W. & Dalton, C. 1999 Numerical prediction of force on rectangular cylinders in oscillating viscous flow. J. Fluids Struct. 13, 225249.Google Scholar

Shao et al. supplementary movie

The evolutions of vortices during t=15T – 40T for Re = 125, θ = 90°, φ0 = 0° and T* = 4.

Download Shao et al. supplementary movie(Video)
Video 3.2 MB

Shao et al. supplementary movie

The evolutions of vortices, showing persistent leftward ejections of the vortex pairs for Re=250, T*= 2, θ = 90° and φ0 = 40°.

Download Shao et al. supplementary movie(Video)
Video 327.1 KB

Shao et al. supplementary movie

The evolutions of vortices during t=17T –27T for Re=250, T*= 2, θ = 90° and φ0= 20°.

Download Shao et al. supplementary movie(Video)
Video 1.3 MB

Shao et al. supplementary movie

The evolutions of vortices during t=70T –80T, showing persistent leftward ejections of the vortex pairs for Re=250, T*= 2, θ = 90° and φ0= 20°.

Download Shao et al. supplementary movie(Video)
Video 1.2 MB

Shao et al. supplementary movie

The motion of the body and evolutions of vortices during t=0 –40T , for Re=250, T*= 2 , θ = 90° , ρr=80 and Fr= 5.85×103.

Download Shao et al. supplementary movie(Video)
Video 2.9 MB