Numerical computation of aerodynamic noise of two tandem circular cylinders and flapping wing motion based on immersed boundary method
With the continuous development of theories, numerical computations and computational conditions, computational aero-acoustics presents huge advantages when they are used to solve the aerodynamic noise. Under low Mach number, objects with complex geometric profiles were selected as the research obje...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
JVE International
2016-12-01
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| Series: | Journal of Vibroengineering |
| Subjects: | |
| Online Access: | https://www.jvejournals.com/article/17188 |