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We find that in a separated flow past a NACA airfoil near the wavy ground at low Reynolds number, the stationary mode is the dominant mode, and the Kelvin-Helmholtz instability is less damped in the range of small wavenumbers.
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This page is a summary of: Stability of Low-Reynolds-Number Separated Flow Around an Airfoil Near a Wavy Ground, AIAA Journal, January 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j057544.
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