The author provides a method and sequence for the analytical calculation of turbine blade throat path dimension.
本文介绍了用解析法计算涡轮叶片喉道尺寸的方法和步骤。
The second crushing blade (2) is adjusted to move substantially harmonically back and forth along a linear path.
第二破碎刀片(2)被调整成沿着一条线性路径进行实质上谐波式往复运动。
The initial path of crack pro-pogation is related with a rake angle of the cutting blade.
裂纹扩展的初期路径与刀具的前角有关。
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