Experimental investigations in low-noise trailing-edge design
By M. Herr, W. Dobrzynski. 2004
256 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Biomedical Engineering, Environmental Engineering
View Paper: https://www.semanticscholar.org/paper/f48e4d3cb70902d4e4dc6e24bfab93952b537715
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In Aerospace Engineering
In Biomedical Engineering
In Environmental Engineering
Citations in the corpus
- Silent Owl Flight: Bird Flyover Noise Measurements (2011, background): “Many of these mechanisms have already been tested for their applicability in technical airfoils, resulting for example in sawtooth [1] or serrated trailing edges [2], comblike or brushlike flow-permeable trailing edges [3,4], or porous airfoils [5,6].”
- Prediction of Wind Turbine Noise and Validation against Experiment (2009, background): “Due to the large number of applications (for example wind turbines, airplanes, helicopters, fans), the characteristics of airfoil noise have been investigated extensively in both experimental and theoretical studies [4–22].”
- Noise-Reduction Mechanism of a Flat-Plate Serrated Trailing Edge (2013, result): “This is in agreement with the findings of Herr and Dobrzynski [26] who also reported flat plate blunt trailing edge vortex shedding noise to occur at Stt ≈ 0.1.”