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Numerical Investigation of an Airfoil with a Gurney Flap

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TLDR
In this paper, the effect of Gurney flaps on the NACA 4412 airfoil was investigated using the one-equation turbulence model of Baldwin and Barth.
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This article is published in Aircraft Design.The article was published on 1998-06-01 and is currently open access. It has received 87 citations till now. The article focuses on the topics: Gurney flap & Aerodynamic center.

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Citations
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Journal ArticleDOI

Gurney flap—Lift enhancement, mechanisms and applications

TL;DR: A review of the characteristics and mechanisms of lift enhancement by the Gurney flap and its applications can be found in this article, where the authors also discuss the application of the GURNey flap to modern aircraft design.
Journal ArticleDOI

Time resolved PIV analysis of flow over a NACA 0015 airfoil with Gurney flap

TL;DR: In this paper, a NACA 0015 airfoil with and without a Gurney flap was studied in a wind tunnel with Re c = 2.0 × 105 and Re c ≥ 0.13.
Journal ArticleDOI

Thin-Airfoil Theoretical Interpretation for Gurney Flap Lift Enhancement

TL;DR: In this article, a thin-airfoil theory is applied to the lift problem of an airfoil with a Gurney flap, and the lift and pitching moment coefficient increments are given as a square-root function of the relative Gurny flap height, and they are proportionally related.
Journal ArticleDOI

On the use of Gurney Flaps for the aerodynamic performance augmentation of Darrieus wind turbines

TL;DR: In this paper, an extended numerical analysis using Computational Fluid Dynamics (CFD) was carried out with the aim of evaluating the potential of using Gurney Flaps for the power augmentation of Darrieus wind turbines.
Journal ArticleDOI

Numerical investigation into energy extraction of flapping airfoil with Gurney flaps

TL;DR: In this paper, a new type of Gurney flap is applied for energy extraction enhancement of a flapping airfoil, which significantly increases the maximum output power and efficiency.
References
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Proceedings ArticleDOI

A one-equation turbulence transport model for high Reynolds number wall-bounded flows

TL;DR: In this article, a one-equation turbulence model that avoids the need for an algebraic length scale is derived from a simplified form of the standard k-epsilon model equations.
Journal ArticleDOI

Design of Subsonic Airfoils for High Lift

TL;DR: In this article, the authors defined the upper surface lift coefficient of an airfoil chord and defined the freestream conditions at the leading edge of the chord line, and the ratio of specific heats.
BookDOI

Numerical Solution of the Incompressible Navier-Stokes Equations

TL;DR: The incompressible Navier-Stokes equations are applied to vorticity-stream function equations, which deal with the role of curvature in the flow of fluid dynamics in two-dimensional systems.

On one-dimensional stretching functions for finite-difference calculations. [computational fluid dynamics]

M. Vinokur
TL;DR: In this paper, the class of one-dimensional stretching functions used in finite-difference calculations is studied for solutions containing a highly localized region of rapid variation, simple criteria for a stretching function are derived using a truncation error analysis.
Journal ArticleDOI

On One-Dimensional Stretching Functions for Finite-Difference Calculations

TL;DR: The class of one-dimensional stretching functions used in finite-difference calculations is studied in this paper, for solutions containing a highly localized region of rapid variation, simple criteria for a stretching function are derived using a truncation error analysis.
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Frequently Asked Questions (1)
Q1. What are the contributions mentioned in the paper "Numerical investigation of an airfoil with a gurney flap" ?

Gurney flap sizes of 0. 5 %, 1. 0 %, 1. 25 %, 1. 5 %, 2. 0 %, and 3. 0 % of the airfoil chord were studied. The numerical solutions show the details of the flow structure at the trailing edge and provide a possible explanation for the increased aerodynamic performance.