Schwartz-Christoffel Panel Method

Autor:	Etsuo Morishita
Rok vydání:	2004
Předmět:	Airfoil Christoffel symbols Numerical analysis Aerospace Engineering Geometry Aerodynamics Geometric shape Physics::Fluid Dynamics Unit circle Transformation (function) Space and Planetary Science Applied mathematics Potential flow Mathematics
Zdroj:	TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 47:153-157
ISSN:	0549-3811
Popis:	The classical Schwartz-Christoffel transformation can be extended to airfoils by a modern computational approach, which otherwise would be limited to calculating potential flows around simple geometric shapes. A numerical method is proposed to determine the Schwartz-Christoffel transformation from a unit circle to paneled general aviation airfoils. The present calculations agree with the theoretical predictions, and they are also compared to experimental results.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::e121576e295d2eb4e72eacec211b4e0b https://doi.org/10.2322/tjsass.47.153 Zobrazit plný text záznamu