Department of Mechanical Engineering, University of Alberta, Edmonton, AB T6G 2R3, Canada.
Department of Mechanical and Mechatronics Engineering, Lakehead University, Thunder Bay ON P7B 5E1, Canada.
J R Soc Interface. 2024 Jul;21(216):20240157. doi: 10.1098/rsif.2024.0157. Epub 2024 Jul 31.
This study introduces novel physics-based scaling laws to estimate the propulsive performance of synchronously pitching foils in various schooling configurations. These relations are derived from quasi-steady lift-based and added mass forces. Hydrodynamic interactions among the schooling foils are considered through vortex-induced velocities imposed on them, constituting the ground effect. Generalized scaling equations are formulated for cycle-averaged coefficients of thrust and power. These equations encompass both the pure-pitching and induced velocity terms, capturing their combined effects. The equations are compared to computational results obtained from two-foil systems, exhibiting foil arrangements over a wide range of parameter space, including Strouhal number (0.15 ≤ ≤ 0.4), pitching amplitude ([Formula: see text]) and phase difference ([Formula: see text]) at = 1000-10 000. The individual contributions of pure-pitching and induced velocity terms to propulsive performance elucidate that solely relying on the pure-pitching terms leads to inadequate estimation, emphasizing the significance of the induced velocity terms. The validity of the approach is further assessed by testing it with three-foil and five-foil configurations, which displays a collapse of estimated and measured results. This indicates that the scaling laws are applicable to multi-foil arrangements.
本研究提出了新颖的基于物理的比例定律,用于估计各种游动配置下同步俯仰翼片的推进性能。这些关系是从准稳态基于升力和附加质量力推导出来的。通过施加于翼片上的涡致速度来考虑游动翼片之间的水动力相互作用,构成了地面效应。为周期平均推力和功率系数制定了广义比例定律。这些方程包含了纯俯仰和诱导速度项,捕捉了它们的综合影响。将这些方程与从双翼系统获得的计算结果进行了比较,展示了在广泛的参数空间中翼片布置的情况,包括斯特劳哈尔数(0.15 ≤ ≤ 0.4)、俯仰幅度([公式:见文本])和相位差([公式:见文本]),[Formula: see text]在 1000-10 000 之间。纯俯仰和诱导速度项对推进性能的单独贡献表明,仅依赖于纯俯仰项会导致估计不足,强调了诱导速度项的重要性。通过对三翼片和五翼片配置进行测试,进一步评估了该方法的有效性,结果显示估计和测量结果的崩溃。这表明这些比例定律适用于多翼片布置。