The effects of turbomachinery blade bow and sweep on aerodynamic loading distribution of the blade are investigated.
研究叶轮机叶片的弯扭及掠形等因素对叶片气动负荷分布的影响。
It is shown that the blade bow, twist and leading edge sweep are effective in adjusting the loading distribution on the blade surface.
分析结果表明，叶轮机叶片的弯扭和前缘掠形对叶片的负荷分布有重要的调节作用。
It is shown that the blade bow, twist and leading edge sweep are effective in adjusting the loading distribution on the blade surface.
分析结果表明，叶轮机叶片的弯扭和前缘掠形对叶片的负荷分布有重要的调节作用。
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