A scaling law for thrust generating unsteady hydrofoils

被引:12
作者
Lau, Timothy C. W. [1 ]
Kelso, Richard M. [1 ]
机构
[1] Univ Adelaide, Sch Mech Engn, Ctr Energy Technol, Adelaide, SA 5005, Australia
关键词
Unsteady foil; Quasi-steady model; Aquatic propulsion; FLAPPING FOIL PROPULSION; OSCILLATING FOILS; DYNAMIC-STALL; FLOW STRUCTURES; ODONTOCETE CETACEANS; VORTICITY CONTROL; PLUNGING AIRFOIL; RAINBOW-TROUT; EFFICIENCY; HYDRODYNAMICS;
D O I
10.1016/j.jfluidstructs.2016.06.015
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
An investigation into the flow around a fully submerged fish-inspired heaving and pitching hydrofoil was performed using a combination of a quasi-steady model, based on classical hydrodynamics, and experimental force measurements. From the quasi-steady model, a scaling law for the time-averaged foil thrust, based on the non-dimensional term St(St - St(0)) where St is the Strouhal number and St(0) is the "neutral force" Strouhal number, was proposed. Experimental force measurements were conducted for a wide range of non-dimensional heave amplitudes, 0.25 <= h(0)/c <= 1, pitch amplitudes, 0 <= theta(0) <= 45 degrees and Strouhal numbers, 0.1 <= St <= 0.95, to confirm the accuracy of the model and scaling law. The Reynolds number for these experiments spanned the range 1500 <= Re <= 12500. For most flow cases, the experimental results show good agreement with the quasi-steady model and show excellent collapse when plotted against the proposed scaling term St(St - St(0)). However, under conditions where unsteady flow dynamics (such as dynamic stall) are expected to be important, i.e. when the non-dimensional heave amplitude is large relative to the pitch amplitude, the experimental results depart from the model and the scaling law. This shows that the quasi-steady model, although simple, is sufficient at predicting the foil thrust development when unsteady effects are small, and that any departure from scaling law can be used to indicate that the flow regime is dominated by a range of unsteady flow effects. (C) 2016 Elsevier Ltd. All rights reserved.
引用
收藏
页码:455 / 471
页数:17
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