Methods and apparatus for structurally supporting airfoil tips
作者： Aspi R. Wadia , Rolf Hetico , Hsin-Yi Yen , Robert Bruce Dickman , Peter Wood
DOI:
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摘要: An airfoil for a gas turbine engine includes leading edge, trailing tip, first side wall that extends in radial span between an root and the wherein defines of said airfoil, second connected to at edge such airfoil. The also rib outwardly from least one wall, natural frequency chordwise vibration is increased not present within during operations.
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