Schwartz-Christoffel Panel Method
Autor: | Etsuo Morishita |
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Rok vydání: | 2004 |
Předmět: | |
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 |
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