Numerical Investigation on the Thrust Vectoring Performance of Bypass Dual Throat Nozzle
Modern aircraft and missiles are gradually integrating thrust vector control systems to enhance their military capabilities. Bypass Dual-Throat Nozzle (BDTN) control is a new fluidic thrust vectoring technique capable of achieving superior performance with large vector angles and low thrust loss. In...
में बचाया:
| मुख्य लेखकों: | , , , , , , |
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| स्वरूप: | Artigo |
| भाषा: | Inglês |
| प्रकाशित: |
MDPI AG
2023-01-01
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| श्रृंखला: | Energies |
| विषय: | |
| ऑनलाइन पहुंच: | https://www.mdpi.com/1996-1073/16/2/594 |
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