日本機械学会論文集 B編
Online ISSN : 1884-8346
Print ISSN : 0387-5016
多翼送風機の空力性能に関する研究 : 第2報,軸動力の予測計算に関する研究
山崎 進佐藤 良次
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1987 年 53 巻 485 号 p. 108-113

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In this paper, prediction of the shaft power is studied. The slip factor and the leakage flow factor used for the performance calculation are obtained experimentaly. The method of prediction of the shaft power is based on the angular momentum theory, and it is derived from measurement of the slip factor, blockage factor and leakage flow. The slip factor is strongly related to the blade angle β2, the number of blades Z and the capacity coefficient φ, and it is smaller than 0.35 at 170 degree of β2, which is much smaller than that for the backward blades. The difference between the calculated values and the experimental results on the shaft power is 5 % for the range of φ less than 0.3 and is 11 % for φ= 0.45.

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