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- W354792285 abstract "Report presenting a review of the possible shock system associated with the supersonic blade elements encountered in transonic-compressor rotors. The variation of shock shape and location with operating conditions is described. Results regarding flow, estimated shock losses at maximum element efficiency, and profile losses are provided." @default.
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- W354792285 date "1957-03-29" @default.
- W354792285 modified "2023-09-26" @default.
- W354792285 title "A preliminary analysis of the magnitude of shock losses in transonic compressors" @default.
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