Undercut leading edge for compressor blades and related method
作者： James Charles Gautreau , Nicholas Francis Martin
DOI:
关键词: Engineering 、 Structural engineering 、 Leading edge 、 Airfoil 、 Front (military) 、 Compressor blade 、 Undercut
摘要: A compressor blade includes an airfoil portion having a leading edge, radially inner attachment portion, and platform between the wherein material is removed from to form undercut at front face thereof thereby provide overhang inward of edge portion.
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