Approximation of free-form curve - Airfoil shape

• Main Authors: Chong, Perk Lin, Cheong, Khai Yip
• Format: Article
• Language: English
• Published: School of Engineering, Taylor’s University 2013
• Subjects: TA Engineering (General). Civil engineering (General)
• Online Access: http://eprints.intimal.edu.my/70/1/Approximation%20of%20free-form%20curve%20-%20Airfoil%20shape.pdf; http://eprints.intimal.edu.my/70/; http://jestec.taylors.edu.my/

Approximation of free-form shape is essential in numerous engineering applications, particularly in automotive and aircraft industries. Commercial CAD software for the approximation of free-form shape is based almost exclusively on parametric polynomial and rational parametric polynomial. The parametric curve is defined by vector function of one independent variable R(u) = (x(u), y(u), z(u)), where 0≤u≤1. Bézier representation is one of the parametric functions, which is widely used in the approximating of free-form shape. Given a string of points with the assumption of sufficiently dense to characterise airfoil shape, it is desirable to approximate the shape with Bézier representation. The expectation is that the representation function is close to the shape within an acceptable working tolerance. In this paper, the aim is to explore the use of manual and automated methods for approximating section curve of airfoil with Bézier representation.