1951
DOI: 10.1299/kikai1938.17.60_1
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Cavitation Tests on Six Profiles for Blade Elements

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“…At this time, an inlet flow velocity is U 0 = 10m/s and a Reynolds number is R e = 7.0 × 10 5 . Time-averaged lift and drag coefficients C L , C D were calculated from numerical results, and the comparison with experimental data at the same Reynolds number(see, for example, Numachi, Tsunoda and Chida(1949)) is shown in Fig.1. Generally, it is known that C L decreases largely when σ becomes smaller than a certain critical value (that is so-called cavitation break-down).…”
Section: Validation Of Present Methods (Comparison With Experimental Rmentioning
confidence: 99%
“…At this time, an inlet flow velocity is U 0 = 10m/s and a Reynolds number is R e = 7.0 × 10 5 . Time-averaged lift and drag coefficients C L , C D were calculated from numerical results, and the comparison with experimental data at the same Reynolds number(see, for example, Numachi, Tsunoda and Chida(1949)) is shown in Fig.1. Generally, it is known that C L decreases largely when σ becomes smaller than a certain critical value (that is so-called cavitation break-down).…”
Section: Validation Of Present Methods (Comparison With Experimental Rmentioning
confidence: 99%