International Journal of Fluid Machinery and Systems
Online ISSN : 1882-9554
Original paper
Inverse Design of Airfoil Using Vortex Element Method
Avinash G.S.S. Anil Lal
Author information

2018 Volume 11 Issue 2 Pages 163-170


A methodology for the parameterization and inverse design of airfoils, for obtaining a given target surface pressure distribution is presented. The airfoil parameterization is carried out using ordered pairs representing the x-y coordinates of ten control points of Bezier curve as parameters. The forward model consists of analysis of flow over airfoils carried out using vortex element method, which involve discretisation of the airfoil curve alone, in contrast to complicated grid generation over the region of flow. The airfoil parameters are selected by global search using a Genetic Algorithm code. Examples to illustrate the parameterization and design of airfoils are presented. A good matching between the target and designed airfoil shows that present methodology can be used as a tool for the design of airfoils.

Information related to the author

This article cannot obtain the latest cited-by information.

© 2018 Turbomachinery Society of Japan, Korean Fluid Machinery Association, Chinese Society of Engineering Thermophysics, IAHR
Previous article Next article