Numerical method to compute acoustic scattering effect of a moving source

In this paper, the aerodynamic characteristic of a ducted tail rotor in hover has been numerically studied using CFD method. An analytical time domain formulation based on Ffowcs Williams–Hawkings (FW–H) equation is derived for the prediction of the acoustic velocity field and used as Neumann bounda...

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Detalles Bibliográficos
Autores principales: Song, Hao, Yi, Mingxu, Huang, Jun, Pan, Yalin, Liu, Dawei
Formato: Online Artículo Texto
Lenguaje:English
Publicado: Springer International Publishing 2016
Materias:
Research
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC4995198/
https://www.ncbi.nlm.nih.gov/pubmed/27610323
http://dx.doi.org/10.1186/s40064-016-3080-x

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC4995198/
https://www.ncbi.nlm.nih.gov/pubmed/27610323
http://dx.doi.org/10.1186/s40064-016-3080-x

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