Direct Numerical Simulations of the Flow Past a Cylinder Moving With Sinusoidal and Nonsinusoidal Profiles

2009 ◽  
Vol 131 (12) ◽  
Author(s):  
Osama A. Marzouk

We perform direct numerical simulations of the flow past a circular cylinder undergoing a one-degree-of-freedom transverse oscillation. The displacement follows a sine function raised to an arbitrary integer power ranging from 1 to 8. When the displacement power is above 2, we have multifrequency oscillation, and the number of Fourier components in the oscillation increases with the power, but they are either odd or even multiples of the input (argument) frequency of the displacement function. We study the responses of the nondimensional lift and drag under these different oscillation profiles and the transfer of nondimensional mechanical energy due to the oscillation, and their trends as the power (hence the number of Fourier components in the oscillation) increases. For odd powers, the energy is transferred to the cylinder; whereas for even powers, it is transferred to the flow. A unity power (harmonic oscillation) corresponds to the maximum energy transfer to the cylinder, which can explain the occurrence of this profile in the case when the cylinder is free to oscillate due to the vortex-induced vibration (VIV) phenomenon. The lift exhibits a mean value only with even powers above 2. The results show that the lift is driven to a large extent by the acceleration of the oscillation rather than its velocity. This should be considered when modeling the fluid-structure coupling in reduced-order VIV models.

2015 ◽  
Vol 12 (113) ◽  
pp. 20150821 ◽  
Author(s):  
Shizhao Wang ◽  
Xing Zhang ◽  
Guowei He ◽  
Tianshu Liu

This paper elucidates the aerodynamic role of the dynamically changing wingspan in bat flight. Based on direct numerical simulations of the flow over a slow-flying bat, it is found that the dynamically changing wingspan can significantly enhance the lift. Further, an analysis of flow structures and lift decomposition reveal that the elevated vortex lift associated with the leading-edge vortices intensified by the dynamically changing wingspan considerably contributed to enhancement of the time-averaged lift. The nonlinear interaction between the dynamically changing wing and the vortical structures plays an important role in the lift enhancement of a flying bat in addition to the geometrical effect of changing the lifting-surface area in a flapping cycle. In addition, the dynamically changing wingspan leads to the higher efficiency in terms of generating lift for a given amount of the mechanical energy consumed in flight.


2021 ◽  
Vol 33 (3) ◽  
pp. 034128
Author(s):  
Yakun Zhao ◽  
Song Gao ◽  
Xiantao Zhang ◽  
Xiaoxian Guo ◽  
Xin Li ◽  
...  

2009 ◽  
Vol 320 (4-5) ◽  
pp. 838-858 ◽  
Author(s):  
R.D. Sandberg ◽  
L.E. Jones ◽  
N.D. Sandham ◽  
P.F. Joseph

2017 ◽  
Vol 72 ◽  
pp. 152-168 ◽  
Author(s):  
Xinliang Tian ◽  
Zhihuan Hu ◽  
Haining Lu ◽  
Jianmin Yang

2019 ◽  
Vol 31 (4) ◽  
pp. 045108 ◽  
Author(s):  
Shashank S. Tiwari ◽  
Shivkumar Bale ◽  
Ashwin W. Patwardhan ◽  
Krishnaswamy Nandakumar ◽  
Jyeshtharaj B. Joshi

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