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2025-01-07 加入
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An Analysis of the Secondary Flow Around a Tandem Blade Under the Presence of a Tip Gap in a High-Speed Linear Compressor Cascade
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Three-dimensional flow investigation of a high-pressure turbine with rotor tip desensitization based on Winglet geometry
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An Analysis of the Secondary Flow Around a Tandem Blade Under the Presence of a Tip Gap in a High-Speed Linear Compressor Cascade
Three-dimensional flow investigation of a high-pressure turbine with rotor tip desensitization based on Winglet geometry
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