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Journal ArticleDOI

Self-sustained aeroelastic oscillations of a NACA0012 airfoil at low-to-moderate Reynolds numbers

Dominique Poirel, +2 more
- 01 Jul 2008 - 
- Vol. 24, Iss: 5, pp 700-719
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TLDR
In this article, a wind tunnel experimental investigation of self-sustained oscillations of an aeroelastic NACA0012 airfoil occurring in the transitional Re regime is presented.
About: 
This article is published in Journal of Fluids and Structures.The article was published on 2008-07-01. It has received 144 citations till now. The article focuses on the topics: Laminar flow & Airfoil.

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Citations
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Journal ArticleDOI

Recent progress in flapping wing aerodynamics and aeroelasticity

Wei Shyy, +6 more
- 01 Oct 2010 - 
TL;DR: In this article, a review of the recent progress in flapping wing aerodynamics and aeroelasticity is presented, where it is realized that a variation of the Reynolds number (wing sizing, flapping frequency, etc.) leads to a change in the leading edge vortex (LEV) and spanwise flow structures, which impacts the aerodynamic force generation.
Journal ArticleDOI

A review on flow energy harvesters based on flapping foils

Qing Xiao, +1 more
- 01 Apr 2014 - 
TL;DR: An overview of the state-of-the-art investigations on the recently developed oscillating foil energy converters is presented in this article, where a summary of available knowledge and up-to-date progress in the application of such bio-inspired systems for renewable energy devices is provided.
Book

An Introduction to Flapping Wing Aerodynamics

Wei Shyy, +3 more
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

Energy harvesting by a purely passive flapping foil from shear flows

Qiang Zhu
- 01 Oct 2012 - 
TL;DR: In this paper, the response of a purely passive flapping foil flow energy harvester in a linear shear flow was investigated using a two-dimensional numerical approach, and the performance of the system, characterized by its energy harvesting efficiency, was found to be comparable to that in the uniform flow case.
Journal ArticleDOI

Flutter and Stall Flutter of a Rectangular Wing in a Wind Tunnel

N. A. Razak, +2 more
- 01 Oct 2011 - 
TL;DR: In this article, the aeroelastic behavior of a rectangular wing with pitch and plunge degrees of freedom was observed experimentally using pressure, acceleration, and particle image velocimetry measurements.
References
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Book

Viscous Fluid Flow

Frank M. White
TL;DR: In this article, the stability of Laminar Boundary Layer Flow Appendices has been investigated in Cylindrical and Spherical Coordinates of Incompressible Newtonian Fluids.

Theory of Wing Sections

Ira H Abbott, +1 more
TL;DR: Chang et al. as discussed by the authors proposed a new geometric analysis procedure for wing sections based on the normal mode analysis for continuous functions, which can be used to calculate the section length.
Book

An introduction to the theory of aeroelasticity

Yuan-Cheng Fung
TL;DR: An introduction to the theory of aeroelasticity, An Introduction to the Theory of Aero-Elasticity as mentioned in this paper, An introduction to aero-elasticities,
Journal ArticleDOI

Low-speed flows involving bubble separations

Itiro Tani
- 01 Jan 1964 - 

Airfoil section characteristics as affected by variations of the Reynolds number

Eastman N Jacobs, +1 more
TL;DR: In this paper, the results of an investigation of a systematically chosen representative group of related airfoils conducted in the NACA variable-density wind tunnel over a wide range of Reynolds number extending well into the flight range are presented.