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Design of Turbine Cascade Blades by Dominant Curvature Method.
被引：0
作者：
Mamaev, B.I.
Ryabov, E.K.
机构：
来源：
Teploenergetika
|
1979年
/
02期
关键词：
D O I：
暂无
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学科分类号：
摘要：
A new method of computer-aided design of the airfoil shape is proposed. Not the contour line itself but a function of its curvature is chosen as the dominant object, which is to be directly determined. This permits reproduction of any character of variation of the curvature along the contour.
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页码：52 / 55
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