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- W2016979186 abstract "In this paper, the author represents the drag coefficients that are necessary when we design an axial-flow compressor. These drag coefficients are based on the data of the single-stage axial-flow blower, which is applied to the measurement of total pressure distribution on the relative flow field in down-stream of the rotating blades by a special technique. From this study, the author proposes new formulas of the drag coefficients as follows : 1) Profile drag coefficient [numerical formula] (Conventional formula) 2) Secondary-flow drag coefficient [numerical formula] 3) Annulus drag coefficient [numerical formula] 4) Tip clearance drag coefficient [numerical formula]" @default.
- W2016979186 created "2016-06-24" @default.
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- W2016979186 date "1962-01-01" @default.
- W2016979186 modified "2023-10-17" @default.
- W2016979186 title "A Study of the Flow through the Rotor of an Axial-Compressor : A Proposition of Formulas of Drag Coefficients" @default.
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- W2016979186 doi "https://doi.org/10.1299/jsme1958.5.292" @default.
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