Airfoil Trailing-Edge Noise Reduction by Application of Finlets
Author:
Affiliation:
1. University of Bristol, Bristol, England BS8 1TR, United Kingdom
Funder
H2020 Environment
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J060699
Reference42 articles.
1. Noise due to turbulent flow past a trailing edge
2. Effect of inclined transverse jets on trailing-edge noise generation
3. REDUCTION OF UNSTEADY STATOR–ROTOR INTERACTION USING TRAILING EDGE BLOWING
4. Influence of boundary layer flow suction on trailing edge noise generation
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