Boundary layer characterization and acoustic measurements of flow-aligned trailing edge serrations
Author:
Funder
Innovation Fund Denmark
Publisher
Springer Science and Business Media LLC
Subject
Fluid Flow and Transfer Processes,General Physics and Astronomy,Mechanics of Materials,Computational Mechanics
Link
http://link.springer.com/article/10.1007/s00348-016-2272-z/fulltext.html
Reference76 articles.
1. Amiet R (1975) Correction of Open Jet Wind tunnel measurements for shear layer refraction. In: 2nd AIAA aeroacoustics conference, Hampton. 24–26 March 1975. doi: 10.2514/6.1975-532
2. Amiet R (1976) Noise due to turbulent flow past a trailing edge. J Sound Vib 47(3):387–393. doi: 10.1016/0022-460X(76)90948-2
3. Arce León C, Ragni D, Pröbsting S, Scarano F, Madsen J (2016) Flow topology and acoustic emissions of trailing edge serrations at incidence. Exp Fluids 57(5):91. doi: 10.1007/s00348-016-2181-1
4. Arina R, Della Ratta Rinaldi R, Iob A, Torzo D (2012) Numerical study of self-noise produced by an airfoil with trailing-edge serrations. In: 18th AIAA/CEAS aeroacoustics conference (33rd AIAA aeroacoustics conference), American Institute of Aeronautics and Astronautics, Colorado Springs, June, pp 4–6. doi: 10.2514/6.2012-2184
5. Arroyo MP, Greated CA (1991) Stereoscopic particle image velocimetry. Meas Sci Technol 2(12):1181–1186. doi: 10.1088/0957-0233/2/12/012
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