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- W2334388314 abstract "In this paper, airfoil-broadband noise at low Mach number and low Reynolds number is experimentaly investigated in the ECL-LMFA open-jet anechoic wind tunnel. The results are focussed on two different airfoils for both self noise and turbulence-interaction noise mechanisms. They are part of a more extended data set on different airfoils, including a flat plate, a NACA 0012 airfoil and other profiles. The airfoil design plays no significant role in the trailing-edge far field noise. In contrast, the thickness at the leading edge is found to have an important effect on the turbulence-interaction noise. Apart from the definition of guidelines for low-noise design, the main goal is to test analytical prediction schemes that can be used as a post processing tool of aerodynamic results obtained by RANS-computations. So numerical simulations of the experiments are performed to provide relevant scaling parameters of the wall pressure spectra." @default.
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- W2334388314 date "2006-05-08" @default.
- W2334388314 modified "2023-10-12" @default.
- W2334388314 title "Effect of Blade Design at Equal Loading on Broadband Noise" @default.
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- W2334388314 doi "https://doi.org/10.2514/6.2006-2563" @default.
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