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pro vyhledávání: '"Brouzet, Davy Joao Etienne"'
Publikováno v:
Center for Turbulence Research, Proceedings of the Summer Program, 2022
Airfoil noise is predicted and analyzed using wall-resolved large-eddy simulations and wavelet transforms for a NACA 0012 airfoil at a Mach number of 0.06 and a Reynolds number of 400,000 using a stair-strip forced transition and a natural transition
Externí odkaz:
http://arxiv.org/abs/2302.05809