Method to maximize resonance-free running range for a turbine blade
作者： Ralph E. Gordon , Loc Duong , Olivier J. Lamicq
DOI:
关键词:
摘要: An airfoil for a gas turbine engine component such as blade is tuned to move its natural frequency outside of which will be excited during expected speed range an associated engine. The about locations the anti-nodes in original design. tuning affects only interfered frequency.
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