Results of a wind tunnel study on the reduction of airfoil self-noise by the application of serrated blade trailing edges
Results of a wind tunnel study on the reduction of airfoil self-noise by the application of serrated blade trailing edges
Date
1996
Authors
Dassen, T.
Parchen, R.
Bruggeman, J.
Hagg, F.
Journal Title
Journal ISSN
Volume Title
Publisher
National Aerospace Laboratory NLR