Two-Dimensional Numerical Modelling of Interaction of Micro-Shock Wave Generated by Nanosecond Plasma Actuators and Transonic Flow
The influence of nanosecond pulse-driven, surface-mounted dielectric barrier discharge(DBD) actuators on a transonic flow is studied numerically. An airfoil representing turbomachinery blades in transonic flow is considered as a test case. A two-dimensional fluidmodel of DBD is used to describe the...
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| Outros Autores: | , |
| Formato: | article |
| Idioma: | eng |
| Publicado em: |
2014
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| Texto completo: | https://hdl.handle.net/10216/106445 |
| País: | Portugal |
| Oai: | oai:repositorio-aberto.up.pt:10216/106445 |