Airfoil Noise Prediction Using Large Eddy Simulation, Euler Equations and Kirchhoff Integral

Topics:
Aerospace and Defense
Tags:
Aerospace & Defense,
Manufacturing,
ONERA
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ONERA

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Overview: This paper describes a new step in the development of a Computational AeroAcoustics (CAA) process whose general long term objective is the numerical prediction of the aerodynamic sound radiated by the airframe of large aircraft at approach, and especially the noise generated by deployed high lift devices such as slats and flaps.

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Format: PDF | Size: 907KB | Date: Feb 2003 | Pages: 12

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