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タイトルA comparison of experimental and theoretical turbulence reduction from screens, honeycomb and honeycomb-screen combinations
著者(英)Brooks, J. D.; Scheiman, J.
著者所属(英)NASA Langley Research Center
発行日1980-01-01
言語eng
内容記述A 1/2-scale model of a portion of the NASA Langley 8-foot transonic pressure tunnel was used to conduct some turbulence reduction research. The experimental results are correlated with various theories. Screens alone reduce axial turbulence more than the lateral turbulence; whereas, honeycomb alone reduce lateral turbulence more than axial turbulence. Because of this difference, the physical mechanism for decreasing turbulence for screens and honeycomb must be completely different. Honeycomb with a downstream screen is an excellent combination for reducing turbulence.
NASA分類RESEARCH AND SUPPORT FACILITIES (AIR)
レポートNO80A26943
AIAA PAPER 80-0433
権利Copyright
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/422468


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