发明名称 |
Wind tunnel with a closed section for aeroacoustic measurements with an anechoic coating |
摘要 |
A wind tunnel with a closed section for aeroacoustic measurements with an anechoic coating including: a) a first cavity having a thickness D1 in a range of 20≰D1≰50 mm filled with a fibrous material with a flow resistance R in a range of 10≰R≰50 kRayl/m; b) a first microperforated panel having a thickness t1 in a range of 0.25≰t1≰0.75 mm and with a perforation percentage p1 in a range of 15%≰p1≰30%; c) a second air cavity having a thickness D2 in a range of 10≰D2≰30 mm; d) a second microperforated panel having a thickness t2 in a range of 0.25≰t2≰0.75 mm and with a perforation percentage p2 in a range of 15%≰p2≰30%. The perforations of the panels can be circular or longitudinal slot-shaped having a diameter d or width w in a range of 0.2≰d, w≰0.5 mm. |
申请公布号 |
US8714003(B2) |
申请公布日期 |
2014.05.06 |
申请号 |
US201013266139 |
申请日期 |
2010.04.28 |
申请人 |
RUIZ VILLAMIL HEIDI LENI;ALVAREZ GONZALEZ JOSE JULIAN;COBO PARRA PEDRO;AIRBUS OPERATIONS, S.L. |
发明人 |
RUIZ VILLAMIL HEIDI LENI;ALVAREZ GONZALEZ JOSE JULIAN;COBO PARRA PEDRO |
分类号 |
G01M9/00 |
主分类号 |
G01M9/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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