日本航空宇宙学会誌
Online ISSN : 2424-1369
Print ISSN : 0021-4663
ISSN-L : 0021-4663
エンジンに結合されたプロペラ性能の迅速自動計算法
安東 茂典加藤 三千代
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1991 年 39 巻 449 号 p. 294-302

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A quick automatic method is presented for evaluating a propeller performance combined to an engine. The formulation is obtained through drastic simplification by retaining the essential parts only. A scheme —“thrust-consistent scheme”— is constructed for the part of propeller analysis. Accuracy-examination has been made both for static and forward moving conditions, and confirmed to be within ten% errors. One example of application to an engine-propeller combination is presented, which shows that the present method is much convenient to select the best set of several parameters such as diameter, solidity, and pitch etc.

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© The Japan Society for Aeronautical and Space Sciences
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