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Gas turbine engine having a mistuned stage
Gas turbine engine having a mistuned stage
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机译:具有不平衡状态的燃气涡轮发动机
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摘要
A stage of a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a row of flow directing components circumferentially disposed about a centerline axis and at least one flow directing component of the row having at least one design characteristic that is dissimilar from a corresponding design characteristic of at least one other flow directing component of the row.
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