Assessment of Noise Reduction Concepts for Leading-Edge Slat Noise
Author:
Affiliation:
1. Florida State University
2. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-3461
Reference29 articles.
1. Almost 40 Years of Airframe Noise Research: What Did We Achieve?
2. Unsteady Flow Computations of a Slat with a Blunt Trailing Edge
3. Computational Aeroacoustic Analysis of Slat Trailing-Edge Flow
4. Investigation of the Unsteady Flow and Noise Generation in a Slat Cove
5. Unsteady characteristics of a slat-cove flow field
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4. Effects of Porous Gap Fillers on 30P30N Leading-Edge Slat Noise. Part I: Surface Pressure and Acoustics;28th AIAA/CEAS Aeroacoustics 2022 Conference;2022-06-13
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