Experiments on radiated noise and vibration from a lifting surface at high Reynolds numbers
One of the main hydroacoustic noise sources from fully submerged lifting surfaces is the unsteady separated turbulent flow near the surface’s trailing edge that produces pressure fluctuations on the surface and induces vibratory motions of the lifting surface itself. However, the hydrodynamic forcin...
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Veröffentlicht in: | The Journal of the Acoustical Society of America 2000-05, Vol.107 (5_Supplement), p.2825-2825 |
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creator | Dowling, David R. Bourgoyne, Dwayne Ceccio, Steve Mathews, Thomas |
description | One of the main hydroacoustic noise sources from fully submerged lifting surfaces is the unsteady separated turbulent flow near the surface’s trailing edge that produces pressure fluctuations on the surface and induces vibratory motions of the lifting surface itself. However, the hydrodynamic forcing and subsequent structural response of lifting surfaces are largely undocumented at the high Reynolds numbers typical of many marine propulsion applications. This talk describes a new experimental effort to identify and experimentally document the turbulent flow, induced surface pressures, structural response, and radiated noise of a hydrofoil at chord-based Reynolds numbers up to 60 million. The experiments are conducted at the US Navy’s Large Cavitation Channel with a two-dimensional test-section-spanning hydrofoil (2.1-m chord, 3.0-m span) at flow speeds from 0.5 to 18 m/s. The foil section is a modified NACA 16 with a flat pressure side. At a zero angle of attack, the lift load on the foil approaches 700 kn. The results presented here cover the first phase of the experiments and illustrate flow-structure coupling phenomena that will be investigated in greater detail in the second phase of experiments planned for later this year. [Work sponsored by ONR, Code 333.] |
doi_str_mv | 10.1121/1.429118 |
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However, the hydrodynamic forcing and subsequent structural response of lifting surfaces are largely undocumented at the high Reynolds numbers typical of many marine propulsion applications. This talk describes a new experimental effort to identify and experimentally document the turbulent flow, induced surface pressures, structural response, and radiated noise of a hydrofoil at chord-based Reynolds numbers up to 60 million. The experiments are conducted at the US Navy’s Large Cavitation Channel with a two-dimensional test-section-spanning hydrofoil (2.1-m chord, 3.0-m span) at flow speeds from 0.5 to 18 m/s. The foil section is a modified NACA 16 with a flat pressure side. At a zero angle of attack, the lift load on the foil approaches 700 kn. The results presented here cover the first phase of the experiments and illustrate flow-structure coupling phenomena that will be investigated in greater detail in the second phase of experiments planned for later this year. 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However, the hydrodynamic forcing and subsequent structural response of lifting surfaces are largely undocumented at the high Reynolds numbers typical of many marine propulsion applications. This talk describes a new experimental effort to identify and experimentally document the turbulent flow, induced surface pressures, structural response, and radiated noise of a hydrofoil at chord-based Reynolds numbers up to 60 million. The experiments are conducted at the US Navy’s Large Cavitation Channel with a two-dimensional test-section-spanning hydrofoil (2.1-m chord, 3.0-m span) at flow speeds from 0.5 to 18 m/s. The foil section is a modified NACA 16 with a flat pressure side. At a zero angle of attack, the lift load on the foil approaches 700 kn. The results presented here cover the first phase of the experiments and illustrate flow-structure coupling phenomena that will be investigated in greater detail in the second phase of experiments planned for later this year. 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However, the hydrodynamic forcing and subsequent structural response of lifting surfaces are largely undocumented at the high Reynolds numbers typical of many marine propulsion applications. This talk describes a new experimental effort to identify and experimentally document the turbulent flow, induced surface pressures, structural response, and radiated noise of a hydrofoil at chord-based Reynolds numbers up to 60 million. The experiments are conducted at the US Navy’s Large Cavitation Channel with a two-dimensional test-section-spanning hydrofoil (2.1-m chord, 3.0-m span) at flow speeds from 0.5 to 18 m/s. The foil section is a modified NACA 16 with a flat pressure side. At a zero angle of attack, the lift load on the foil approaches 700 kn. The results presented here cover the first phase of the experiments and illustrate flow-structure coupling phenomena that will be investigated in greater detail in the second phase of experiments planned for later this year. 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title | Experiments on radiated noise and vibration from a lifting surface at high Reynolds numbers |
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