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
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