Nonlinear response of passively flapping foils

被引:4
作者
Farooq, Hamayun [1 ]
Khalid, Muhammad Saif Ullah [2 ]
Akhtar, Imran [3 ]
Hemmati, Arman [2 ]
机构
[1] Bahauddin Zakariya Univ BZU, Ctr Adv Studies Pure & Appl Math CASPAM, Multan 60800, Pakistan
[2] Univ Alberta, Dept Mech Engn, Edmonton, AB T6G 1H9, Canada
[3] Natl Univ Sci & Technol, NUST Coll Elect & Mech Engn, Dept Mech Engn, Islamabad 44000, Pakistan
关键词
Fluid-structure interaction; Nonlinear dynamics; Computational modeling; Flapping foil; Bio-inspiration; VORTEX-INDUCED VIBRATIONS; POWER-EXTRACTION; ENERGY EXTRACTION; OPTIMIZATION; DEFORMATION; SIMULATION; AIRFOIL; MODEL;
D O I
10.1016/j.oceaneng.2022.112071
中图分类号
U6 [水路运输]; P75 [海洋工程];
学科分类号
0814 ; 081505 ; 0824 ; 082401 ;
摘要
This study numerically investigates two-dimensional incompressible flows over elastically mounted foils, undergoing semi-passive and fully passive motion. In our strongly coupled numerical models, we employ linear and cubic stiffness and damping terms in order to examine their highly nonlinear response. The undamped model of the fully passive system exhibits various responses from periodic to chaotic and then to flip-over for the reduced velocity, ranging from 1 to 10. However, introducing the cubic damping terms causes a significant decrease in the magnitude of plunging and pitching amplitudes without affecting the onset point of bifurcation. Also, plunging and pitching amplitudes are altered significantly after the point of onset. Furthermore, the performance metrics of each passive system are computed for power generation applications to demonstrate that semi-passive system attain efficiency up to 20% for a pitching amplitude of 50 with the excitation frequency in the narrow range of 0.15 to 0.20. On the other hand for a fully passive system, the efficiency of around 34% is obtained near the onset point of a bifurcation with a low mass ratio and linear damping terms. However, introducing cubic damping terms causes degradation in efficiency to bring it down to 14 - 20% for a wide range of reduced velocity.
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页数:17
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