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- W2317852456 abstract "This paper describes the numerical analysis on the generation mechanism of discrete tone noise radiated from a two-dimensional wing immersed in uniform flow. Linearized approximate equation of the small perturbation of the boundary layer flow is introduced to the interactive dynamical model between the perturbed flow on the suction side of an airfoil and the sound near field emitted from the trailing edge. The numerical solution of the Green function of the Fourier-Laplace transformation of the perturbed flow variables is derived given the mean velocity profile of the boundary layer. The solution estimates well the configuration of the perturbed flow development." @default.
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- W2317852456 date "2000-01-01" @default.
- W2317852456 modified "2023-09-26" @default.
- W2317852456 title "Discrete Tone Noise on Two-Dimensional Wing. Numerical Analysis on Boundary Layer Instability on Wing." @default.
- W2317852456 doi "https://doi.org/10.1299/kikaib.66.648_2056" @default.
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