blade section camber 叶片截面弯度
blade root blade section blast 喷丸
blade-section chord 叶片剖面弦长
faced blade section 凹面翼断面
blade-section camber 叶剖面曲度
airfoil blade section 翼型桨叶剖面
blade section profile 叶片截面线型
cambered blade section 弯曲桨叶型
Since this method adopts non-linearized theory of the lift coefficient curve of the blade section and multiple streamtube model, and has revised the aspect ratio influence, so it has wide suitability.
这个方法采用了叶型升力曲线的非线性理论和多流管的理论模型,并对展弦比的影响进行了修正,从而具有广泛的适用性。
Besed on theoretic analysis of tube shearing, this paper mainly discusses the design principles and method of tube shearing blade and briefly introduces the design of section shearing blade.
在对剪管工艺作详细理论分析的基础上,重点介绍了剪切圆管的刀片设计原理及方法,并简要介绍了剪切型材的刀片设计。
The experiment has studied the heat transfer characteristic inside U shaped variable cross-section channels with different rib pitches, The channel is the middle part of a gas turbine blade.
本实验选取航空发动机涡轮叶片中段内部冷却通道为研究对象,对不同肋间距的横肋变截面U型通道的换热特性进行了研究。
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