Results of a wind tunnel study on the reduction of airfoil self-noise by the application of serrated blade trailing edges

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TP-1996-350.pdf (250.14 KB)
Date
1996
Authors
Dassen, T.
Parchen, R.
Bruggeman, J.
Hagg, F.
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National Aerospace Laboratory NLR
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http://hdl.handle.net/10921/1359
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