Journal ArticleDOI
Numerical simulation of incompressible viscous flow past a heaving airfoil
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In this article, numerical simulations of a heaving airfoil undergoing non-sinusoidal motions in an incompressible viscous flow are presented, and the wake patterns, thrust force coefficients, and propulsive efficiency at various values of non-dimensional heave velocity are computed.Abstract:
Numerical simulations of a heaving airfoil undergoing non-sinusoidal motions in an incompressible viscous flow is presented In particular, asymmetric sinusoidal motions, constant heave rate oscillations, and sinusoidal motions with a quiescent gap, are considered The wake patterns, thrust force coefficients, and propulsive efficiency at various values of non-dimensional heave velocity are computed These have been compared with those of corresponding sinusoidal heaving motions of the airfoil It is shown that for a given non-dimensional heave velocity and reduced frequency of oscillation, asymmetric sinusoidal motions give better thrust and propulsive efficiencies in comparison to pure harmonic motion On the other hand, constant rate heave motion do not compare favourably with harmonic motion A train of sinusoidal pulses separated by a quiescent gap compares favourably with a pure sinusoidal motion, but with the notable exception that the quiescent gap induces a discontinuity that induces large impulses to the wake patternread more
Citations
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Journal ArticleDOI
Study of mechanisms and factors that influence the formation of vortical wake of a heaving airfoil
Z. C. Zheng,Zhenglun Alan Wei +1 more
TL;DR: In this paper, a two-dimensional numerical study is performed to investigate the relation between the direction of a deflected wake and the vortex pairing mechanisms, and the deflection angle can be correlated with two effective phase velocities defined to represent the trends of symmetry breaking and symmetry holding, respectively.
Journal ArticleDOI
Numerical investigation of angle of attack profile on propulsion performance of an oscillating foil
Qing Xiao,Wei Liao +1 more
TL;DR: In this paper, the effects of effective angle of attack (AOA) profile on an oscillating foil thrust performance were studied using a computational method. And the authors found that the degradation of thrust force and efficiency with sinusoidal pitching/plunging oscillation, at higher St, is effectively alleviated or removed when the AOA is imposed as a cosine profile.
Journal ArticleDOI
Numerical investigations into the asymmetric effects on the aerodynamic response of a pitching airfoil
TL;DR: In this article, the effects of asymmetric sinusoidal motion on pitching airfoil aerodynamics were studied by numerical simulations for 2-D flow around a NACA0012 airframe at Re=1.35×105.
Journal ArticleDOI
Mechanisms of wake deflection angle change behind a heaving airfoil
Zhenglun Alan Wei,Z.C. Zheng +1 more
TL;DR: In this article, an immersed-boundary numerical method is applied to simulate the wake downstream of a two-dimensional heaving airfoil, and a cross-flow effective phase velocity is introduced to analyze the already-formed asymmetric wake behind the air-foil.
Journal ArticleDOI
Numerical study of asymmetric effect on a pitching foil
Qing Xiao,Wei Liao +1 more
TL;DR: In this paper, numerically the effect of asymmetric sinusoidal oscillating motion on the propulsion performance of a pitching foil and attempts to gain insight in whether the low thrust generated by pure pitching could be improved by asymmetric motion.
References
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