Experimental Research on Noise Reduction for Continuous Transonic Wind Tunnel Loop

The noise level of wind tunnel test section is respected as one of the most important performance specifications to represent the flow field quality, especially for large scale wind tunnel. According to the acoustic experimental research conducted in the 0.6 m continuous transonic wind tunnel of CAR...

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Format: Article
Language:zho
Published: EDP Sciences 2020-08-01
Series:Xibei Gongye Daxue Xuebao
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Online Access:https://www.jnwpu.org/articles/jnwpu/full_html/2020/04/jnwpu2020384p855/jnwpu2020384p855.html
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description The noise level of wind tunnel test section is respected as one of the most important performance specifications to represent the flow field quality, especially for large scale wind tunnel. According to the acoustic experimental research conducted in the 0.6 m continuous transonic wind tunnel of CARDC, main noise sources in the tunnel loop included the compressor, the high-speed diffuser and the test section. To reduce the noise in the test section, it is necessary to prevent the test section from the compressor noise propagated both forward and backward. In 0.6 m wind tunnel loop, acoustic treatments were installed on both the compressor rear cone and the fourth corner to prevent the noise emitted from the compressor from propagating forward. The vanes in the forth corner were filled with glass fibers and covered with perforated panels. And the compressor rear cone was covered with three layers of micro-perforated panels. With acoustic treatment in the tunnel loop and the second throat throttling, the fluctuation pressure coefficient (ΔCp) is lower than 0.8%, which is close to the international advanced level.
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spelling doaj.art-0b2425b8b3f04b458d83e2eacc5bd8172023-10-02T00:19:37ZzhoEDP SciencesXibei Gongye Daxue Xuebao1000-27582609-71252020-08-0138485586110.1051/jnwpu/20203840855jnwpu2020384p855Experimental Research on Noise Reduction for Continuous Transonic Wind Tunnel Loop012State Key Laboratory of Aerodynamics, China Aerodynamics Research and Development CenterState Key Laboratory of Aerodynamics, China Aerodynamics Research and Development CenterState Key Laboratory of Aerodynamics, China Aerodynamics Research and Development CenterThe noise level of wind tunnel test section is respected as one of the most important performance specifications to represent the flow field quality, especially for large scale wind tunnel. According to the acoustic experimental research conducted in the 0.6 m continuous transonic wind tunnel of CARDC, main noise sources in the tunnel loop included the compressor, the high-speed diffuser and the test section. To reduce the noise in the test section, it is necessary to prevent the test section from the compressor noise propagated both forward and backward. In 0.6 m wind tunnel loop, acoustic treatments were installed on both the compressor rear cone and the fourth corner to prevent the noise emitted from the compressor from propagating forward. The vanes in the forth corner were filled with glass fibers and covered with perforated panels. And the compressor rear cone was covered with three layers of micro-perforated panels. With acoustic treatment in the tunnel loop and the second throat throttling, the fluctuation pressure coefficient (ΔCp) is lower than 0.8%, which is close to the international advanced level.https://www.jnwpu.org/articles/jnwpu/full_html/2020/04/jnwpu2020384p855/jnwpu2020384p855.htmlcontinuous wind tunneltransonic wind tunnelnoise reductionexperimentacoustic treatment
spellingShingle Experimental Research on Noise Reduction for Continuous Transonic Wind Tunnel Loop
Xibei Gongye Daxue Xuebao
continuous wind tunnel
transonic wind tunnel
noise reduction
experiment
acoustic treatment
title Experimental Research on Noise Reduction for Continuous Transonic Wind Tunnel Loop
title_full Experimental Research on Noise Reduction for Continuous Transonic Wind Tunnel Loop
title_fullStr Experimental Research on Noise Reduction for Continuous Transonic Wind Tunnel Loop
title_full_unstemmed Experimental Research on Noise Reduction for Continuous Transonic Wind Tunnel Loop
title_short Experimental Research on Noise Reduction for Continuous Transonic Wind Tunnel Loop
title_sort experimental research on noise reduction for continuous transonic wind tunnel loop
topic continuous wind tunnel
transonic wind tunnel
noise reduction
experiment
acoustic treatment
url https://www.jnwpu.org/articles/jnwpu/full_html/2020/04/jnwpu2020384p855/jnwpu2020384p855.html