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AIAA Journal. 1992;30(3):697-702. doi: 10.2514/3.10974 Q13.22025

Effect of airfoil (trailing-edge) thickness on the numerical solution of panel methods based on the Dirichlet boundary condition

翼型(后缘)厚度对基于狄利克雷边界条件的面元法数值解的影响

YON, STEVEN; KATZ, JOSEPH; PLOTKIN, ALLEN

DOI: 10.2514/3.10974

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Copyright © AIAA Journal. 中文内容为AI机器翻译,仅供参考!

期刊名:Aiaa journal

缩写:AIAA J

ISSN:0001-1452

e-ISSN:1533-385X

IF/分区:3.2/Q1

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Effect of airfoil (trailing-edge) thickness on the numerical solution of panel methods based on the Dirichlet boundary condition