Maximum-Thrust Nozzle Based on Height Constraints
Compared to conventional aircraft, hypersonic aircraft place a greater emphasis on the integration of aircraft and engines to meet their high-performance requirements. The design challenges of the nozzle are evident in the requirement of a significant area ratio between the inlet and outlet, as well...
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| Principais autores: | , , |
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| Format: | Artigo |
| Sprog: | Inglês |
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MDPI AG
2023-11-01
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| Serier: | Aerospace |
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| Online adgang: | https://www.mdpi.com/2226-4310/10/12/976 |
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