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...
| 發表在: | Energies |
|---|---|
| Main Authors: | Saadia Afridi, Tariq Amin Khan, Syed Irtiza Ali Shah, Taimur Ali Shams, Kashif Mehmood, Wei Li, David Kukulka |
| 格式: | Article |
| 語言: | 英语 |
| 出版: |
MDPI AG
2023-01-01
|
| 主題: | |
| 在線閱讀: | https://www.mdpi.com/1996-1073/16/2/594 |
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