Direct Noise Computation around a 3-D NACA 0012 airfoil-Reference-Cited by-同舟云学术

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Direct Noise Computation around a 3-D NACA 0012 airfoil

Published:2006-05-08 Issue: Volume: Page:
ISSN:
Container-title:12th AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference)
language:
Short-container-title:

Author:

Marsden Olivier¹,Bogey Christophe¹,Bailly Christophe¹

Affiliation:

1. Laboratoire de Mécanique des Fluides et d'Acoustique

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-2503

Reference31 articles.

1. On using large-eddy simulation for the prediction of noise from cold and heated turbulent jets

2. A family of low dispersive and low dissipative explicit schemes for flow and noise computations

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1. A Different Intermittency Formulation for Flow at Low Reynolds Numbers;AIAA SCITECH 2023 Forum;2023-01-19

2. Noise reduction mechanisms for insert-type serrations of the NACA-0012 airfoil;Journal of Fluid Mechanics;2022-05-09

3. Aeroacoustic Investigation of Trailing-Edge Finlets;Advances in Aerospace Science and Technology;2022

4. Computational fluid dynamics investigation into flow behavior and acoustic mechanisms at the trailing edge of an airfoil;Noise & Vibration Worldwide;2018-01

5. Three-dimensional suction flow control and suction jet length optimization of NACA 0012 wing;Meccanica;2015-01-23

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