What is it about?
The mechanism of the slat noise is very complicated because of the complex flow. The noise generated from the 30P30N high-lift airfoil is simulated with a high order spectral difference solver in this study. The tone noise source is studied by analyzing the correlation between the dynamic pressure on the slat cove surface and the near field noise.
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This page is a summary of: Numerical Simulation of the 30P30N High-Lift Airfoil Noise with Spectral Difference Method, AIAA Journal, June 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j058060.
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