2004
DOI: 10.1115/1.1627835
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An Experimental Study of Unsteady Partial Cavitation

Abstract: Unsteady partial cavitation can cause damage to hydraulic machinery and understanding it requires knowledge of the basic physics involved. This paper presents the main results of a research program based on wall-pressure measurements aimed at studying unsteadiness in partial cavitation. Several features have been pointed out. For cavity lengths that did not exceed half the foil chord the cavity was stated to be stable. At the cavity closure a peak of pressure fluctuations was recorded originating from local ca… Show more

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Cited by 220 publications
(117 citation statements)
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“…These excellent results obtained for 2-D cavitating flow confirm the correct assumptions of the proposed numerical model in terms of vaporization and condensation processes, and to verify it's performance with 3-D considerations, we present in the next some numerical results compared to experimental measurement [16] for cavitating flow around hydrofoil NACA66 (Fig 10). In this section, a numerical simulation was performed to further study the performance of the proposed model and unsteady three-dimensional, the choice is justified because of the availability of experimental measurements.…”
Section: D Configuration(naca66mod)mentioning
confidence: 68%
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“…These excellent results obtained for 2-D cavitating flow confirm the correct assumptions of the proposed numerical model in terms of vaporization and condensation processes, and to verify it's performance with 3-D considerations, we present in the next some numerical results compared to experimental measurement [16] for cavitating flow around hydrofoil NACA66 (Fig 10). In this section, a numerical simulation was performed to further study the performance of the proposed model and unsteady three-dimensional, the choice is justified because of the availability of experimental measurements.…”
Section: D Configuration(naca66mod)mentioning
confidence: 68%
“…This different ways of cavities shedding have an important influence on the pressure field at the hydrofoil wall, and there are characterized by the temporal evolution of the lift coefficient Cl compared to experimental result [16] …”
Section: D Configuration(naca66mod)mentioning
confidence: 99%
“…The transducers locations were aligned along the chord on the suction side of the hydrofoil at mid-span, starting from the foil leading edge at a reduced coordinate of x/c = 0.1 to the trailing edge at x/c = 0.9, with increments of 0.1 c. Lift and drag were measured using a resistive gauge hydrodynamic balance with a range up to 1500 N in lift and 150 N in drag. Readers should refer to [3,44] for additional details about the rigid hydrofoil experimental setup and results. The experimental results presented in this paper are taken from [3] for cases with steady sheet cavitation and from [44] for cases with unsteady sheet/cloud cavitation.…”
Section: Fig 2 Hydrofoil Instrumentation and Tunnel Test Section [43]mentioning
confidence: 99%
“…Readers should refer to [3,44] for additional details about the rigid hydrofoil experimental setup and results. The experimental results presented in this paper are taken from [3] for cases with steady sheet cavitation and from [44] for cases with unsteady sheet/cloud cavitation.…”
Section: Fig 2 Hydrofoil Instrumentation and Tunnel Test Section [43]mentioning
confidence: 99%
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