Control of shockwave-boundarylayer-interaction using MEMS plasma devices
US8196871B2 · kind B2 · utility
5Cited by
5References
8Claims
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Key dates
| Filing date | Nov 26, 2008 |
| Grant date | Jun 12, 2012 |
| Priority date | — |
| Expiry date | Feb 20, 2031 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A micro-electromechanical system (MEMS) dielectric barrier discharge (DBD) based aerodynamic actuator is configured to modify a shockwave boundary layer interaction and limit incident boundary layer growth caused by a reflected shockwave.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.