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Numerical methodology for the computation of the sound generated by a non-isothermal mixing layer at low Mach number
- Source :
- Direct and Large-Eddy Simulation VI ISBN: 9781402049095, Proc. 6th Ercoftac Workshop DLES-6, Poitiers, France, 12-14 septembre 2005.
- Publication Year :
- 2005
- Publisher :
- HAL CCSD, 2005.
-
Abstract
- The sound generated by an isothermal and a non-isothermal mixing layer is computed by two methods : an aeroacoustic direct computation and an aeroacoustic hybrid method composed of a quasi-incompressible simulation coupled with the linearized Euler’s equations. A flow configuration that allows quantitative comparisons in the space-time domain is established. The good agreement found between the evolution of the computed flows allows comparisons of the radiated fields in terms of acoustic amplitude and directivity patterns, opening the analysis of incompressible acoustic source terms.
Details
- Language :
- English
- ISBN :
- 978-1-4020-4909-5
- ISBNs :
- 9781402049095
- Database :
- OpenAIRE
- Journal :
- Direct and Large-Eddy Simulation VI ISBN: 9781402049095, Proc. 6th Ercoftac Workshop DLES-6, Poitiers, France, 12-14 septembre 2005.
- Accession number :
- edsair.doi.dedup.....2a26e85d66886ab442324ffe03b294a0