CFD-Driven Enhancement for Supersonic Aircraft Variable Geometry Inlet
High-speed propulsion systems require supersonic inlets for operation; however, these inlets lose efficiency when the flight speed range is wide. Fixed-geometry inlets designed for particular conditions encounter operational difficulties when running at supercritical speeds, including shockwave inst...
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| Autori principali: | , |
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| Natura: | Artigo |
| Lingua: | Inglês |
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MDPI AG
2025-09-01
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| Serie: | Applied Sciences |
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| Accesso online: | https://www.mdpi.com/2076-3417/15/17/9825 |
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