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A MODIFICATION TO THIN-AIRFOIL-SECTION THEORY, APPLICABLE TO ARBITRARY AIRFOIL SECTIONS, TO ACCOUNT FOR THE EFFECTS OF THICKNESS ON THE LIFT DISTRIBUTION

机译：对适用于任意翼型部分的薄翼部分理论进行修改，以便对提升分布的厚度影响进行会计处理

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The method of accounting for the effect of -thickness on the lift distribution given in MCA Report 833, 1945, has been modified. Comparison of lift distributions calculated "by the methods of the present report and KACA Report 833 together with experimental distributions are presented. The results show that the modification improves the predictions of lift distributions for both angle of attack and camber.

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David Graham;
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年度 1951
页码 1-19
总页数 19
原文格式 PDF
正文语种 eng
中图分类工业技术;
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A MODIFICATION TO THIN-AIRFOIL-SECTION THEORY, APPLICABLE TO ARBITRARY AIRFOIL SECTIONS, TO ACCOUNT FOR THE EFFECTS OF THICKNESS ON THE LIFT DISTRIBUTION

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