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Influences of attack angle and mach number on aerodynamic characters of typical sections of extra-long blade in a steam turbine

机译:攻角和马赫数对汽轮机超长叶片典型截面空气动力特性的影响

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摘要

On super-sonic or trans-sonic planar cascade wind tunnel of free jet intermittent type, wind blowing experiments were performed on the typical sections of stator and rotor blades in the last stage of ultra-ultra-critical steam turbine with extra-long blade of 1200mm. The influences of attack angle and Mach number on the aerodynamic performances of these sections of the blade profiles were verified, and their operating ranges were also specified.
机译:在自由射流间歇式超音速或跨音速平面叶栅风洞中,对超长临界汽轮机超末级汽轮机末级的静叶和转子叶片的典型部分进行了吹气实验。 1200毫米验证了攻角和马赫数对叶片轮廓这些部分的空气动力性能的影响,并指定了它们的工作范围。

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