NASA NTRS · 19930035180
A new technique for aerodynamic noise calculation
Abstract
A novel method for the numerical analysis of aerodynamic noise generation is presented. The method involves first solving for the time-dependent incompressible flow for the given geometry. This fully nonlinear method that is tailored to extract the relevant acoustic fluctuations seems to be an efficient approach to the numerical analysis of aerodynamic noise generation.
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Hardin, J. C., Pope, D. S.. 1992-01-01. A new technique for aerodynamic noise calculation. https://ntrs.nasa.gov/citations/19930035180
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