Control of a Supersonic Inlet in Off-Design Conditions with Plasma Actuators and Bleed
Supersonic inlets are a key component of present and future air-breathing propulsion systems for high-speed flight. The inlet design is challenging because of several phenomena that must be taken under control: shock waves, boundary layer separation and unsteadiness. Furthermore, the intensity of th...
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| Format: | Article |
| Language: | English |
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MDPI AG
2020-03-01
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| Series: | Aerospace |
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| Online Access: | https://www.mdpi.com/2226-4310/7/3/32 |