日本航空學會誌
Online ISSN : 1883-5422
プロペラの翼端及び翼數の理論的考察
河田 三治
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ジャーナル フリー

1936 年 3 巻 20 号 p. 1330-1338

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The formula for the calculation of the velocity induced by a finite number of helical vortices was introduced by the author some time ago in this journal. Making use of this result the author put forwards here an approximative method for the calculation of the propeller charac-teristics of any number of blades. The theoretical results were finally compared with the experiment.

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© The Japan Society for Aeronautical and Space Sciences
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