Compressor rotor blade undercut
作者： Ravichand Brahmasuraih
DOI:
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摘要: A rotor blade for an axial compressor that may include airfoil, which includes a leading edge, and root, platform, the platform being outer radial face of root from airfoil extends, dovetail, dovetail including leading-face, is generally points up-stream once installed in compressor. The undercut groove formed on leading-face undercuts at least partially intersection edge platform.
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