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Two-dimensional airfoil shape optimization for airfoils at low speeds

AIAA Modeling and Simulation Technologies Conference, 2012
This paper presents a fast methodology for the design of two-dimensional low-speed airfoils. We propose a methodology in which the design process starts from an already known airfoil or from a new defined airfoil by imposing some basic geometrical characteristics, such as: the airfoil’s radius at the leading edge, the maximum height of the airfoil’s ...
Paul Silisteanu, Ruxandra Botez
openaire   +1 more source

Optimization of flatback airfoils for wind turbine blades

Aircraft Engineering and Aerospace Technology, 2010
PurposeIn recent years, the airfoil sections with blunt trailing edge (called flatback airfoils) have been proposed for the inboard regions of large wind‐turbine blades because they provide several structural and aerodynamic performance advantages. The purpose of this paper is to optimize the shape of these airfoils for optimal performance using a ...
Xiaomin Chen, Ramesh Agarwal
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On the Optimal Control Method for Airfoil and Cascade Analysis

SIAM Journal on Scientific Computing, 1995
Summary: In solving the full potential equation, the least-squares technique provides a robust and efficient approach. In this paper, this approach is investigated and a new algorithm is proposed. In particular, the upwind density technique is used instead and a very effective way of handling the circulation is proposed.
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Airfoil Topology Optimization using Teaching-Learning based Optimization

International Journal of Applied Metaheuristic Computing, 2015
This paper primarily deals with the optimization of airfoil topology using teaching-learning based optimization, a recently proposed heuristic technique, investigating performance in comparison to Genetic Algorithm and Particle Swarm Optimization. Airfoil parametrization and co-ordinate manipulations are accomplished using piecewise b-spline curves ...
Dushhyanth Rajaram   +2 more
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Airfoil Optimization based on Isogeometric Discontinuous Galerkin

Proceedings of the 2018 2nd International Conference on Algorithms, Computing and Systems, 2018
In this paper, an adjoint-based airfoil optimization algorithm is developed based on isogeometric discontinuous Galerkin (IDG) method for compressible Euler equations. We first parameterize the airfoil by B-spline curve approximation with some control points viewed as design variables, and build the B-spline representation of the flow field with the ...
Kun Wang 0054, Shengjiao Yu, Tiegang Liu
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A Novel Global Optimization Algorithm and Its Application to Airfoil Optimization

Journal of Turbomachinery, 2014
In this paper, a novel global optimization algorithm has been developed, which is named as particle swarm optimization combined with particle generator (PSO–PG). In PSO–PG, a PG was introduced to iteratively generate the initial particles for PSO. Based on a series of comparable numerical experiments, it was convinced that the calculation accuracy of ...
B. Yang   +5 more
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An airfoil parameterization method for the representation and optimization of wind turbine special airfoil

Journal of Thermal Science, 2015
A new airfoil shape parameterization method is developed, which extended the Bezier curve to the generalized form with adjustable shape parameters. The local control parameters at airfoil leading and trailing edge regions are enhanced, where have significant effect on the aerodynamic performance of wind turbine.
Yixiong Liu, Ce Yang, Xiancheng Song
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Deep neural network for airfoil optimization

AIAA SCITECH 2022 Forum, 2022
Wenhui Peng, Yao Zhang, Michel Desmarais
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Horizontal Axis Hydroturbine Shroud Airfoil Optimization

2014
The present work concerns the optimization of the shroud of an horizontal axis hydro turbine (HAHT). The main aim is to improve the hydro-turbine efficiency by designing a new shroud airfoil through an optimization process that maximize, as objective function, the power coefficient.
E. Ferrauto, E. Daniele, COIRO, DOMENICO
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Direct Optimization of Transonic Airfoils

1997
The paper reports on the numerical procedure for the optimization of transonic airfoils developed in ALN D.V.D. within BRITE/EURAM AERO-0026 contract. Results for the solution of test case T6 of the workshop are presented.
openaire   +1 more source

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