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Journal ArticleDOI

Reynolds number, thickness and camber effects on flapping airfoil propulsion

TLDR
The effect of varying airfoil thickness and camber on plunging and combined pitching and plunging propulsion at Reynolds number Re=200, 2000, 20,000 and 2×10 6 was studied by numerical simulations for fully laminar and fully turbulent flow regimes as mentioned in this paper.
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This article is published in Journal of Fluids and Structures.The article was published on 2011-02-01. It has received 130 citations till now. The article focuses on the topics: NACA airfoil & Airfoil.

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Citations
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An Introduction to Flapping Wing Aerodynamics

TL;DR: In this article, the authors present an ideal book for graduate students and researchers interested in the aerodynamics, structural dynamics and flight dynamics of small birds, bats and insects, as well as of micro air vehicles (MAVs).
Journal ArticleDOI

A review on fluid dynamics of flapping foils

TL;DR: The fluid dynamics of flapping foils are reviewed in this paper, where a wide range of researches are conducted for the two-dimensional flapping foil which has a relatively simple geometry, however, for a three-dimensional foil, the aspect ratio and shape take effects and completely distinct fluid dynamics are revealed compared with the 2D one.
Journal ArticleDOI

Three-dimensional vortex formation on a heaving low-aspect-ratio wing: Computations and experiments

TL;DR: In this article, the three-dimensional unsteady separation process induced by large-amplitude heaving oscillations of a low-aspect-ratio wing under low-Reynolds-number conditions is investigated.
Journal ArticleDOI

On numerical modeling of animal swimming and flight

TL;DR: A review of the recent progress in numerical techniques of solving animal swimming and flight problems can be found in this paper, where the authors classified numerical studies into five stages, of which the main characteristics and the numerical strategies are described and discussed.
Journal ArticleDOI

Numerical study of large amplitude, nonsinusoidal motion and camber effects on pitching airfoil propulsion

TL;DR: In this article, the effects of large amplitude and nonsinusoidal motion on pitching airfoil aerodynamics for thrust generation were numerically studied with a 2-D NACA0012 and NACA asymmetric airfoils were applied for camber effect study.
References
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Turbulence modeling for CFD

TL;DR: In this paper, the authors proposed a compressible ecoulement for compressible ECCs, based on the disquette reference record created on 2005-11-18, modified on 2016-08-08.
Journal ArticleDOI

Oscillating foils of high propulsive efficiency

TL;DR: In this article, the phase angle between transverse oscillation and angular motion is the critical parameter affecting the interaction of leading-edge and trailing-edge vorticity, as well as the efficiency of propulsion.
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Optimal Thrust Development in Oscillating Foils with Application to Fish Propulsion

TL;DR: In this paper, it was shown that a stable coexistence of the jet profile and the large-scale patterns is ensured only at the frequency of maximum amplification, hence at this frequency optimal efficiency is obtained, i.e., maximum thrust per unit input energy.
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Flapping and flexible wings for biological and micro air vehicles

TL;DR: In this paper, the scaling laws of biological and micro-air vehicles involving wing span, wing loading, vehicle mass, cruising speed, flapping frequency, and power are summarized and discussed.
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