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Numerical Simulation of Landing Gear Noise via Weakly Coupled CFD-CAA Calculations
2013
19th AIAA/CEAS Aeroacoustics Conference
unpublished
The present work is relevant from the numerical prediction of aircraft noise via aeroacoustics hybrid methods. It is part of a more extensive effort, which final objective is the development of a robust and accurate CFD-CAA weak coupling methodology. Within this framework, we focus here on the so-called surface coupling approach, a technique that allows conducting weakly coupled CFD-CAA calculations. Such approach (which had been previously developed and validated on simpler cases) is here
doi:10.2514/6.2013-2068
fatcat:iaqbnn5xvrgjfdypvozu2672tm