Acta Aeronautica et Astronautica Sinica ›› 2025, Vol. 46 ›› Issue (8): 631086.doi: 10.7527/S1000-6893.2024.31086
• special column • Previous Articles
Lixiang WEI1,2,3, Jinglei XU1,2,3(
), Kuangshi CHEN1,2,3, Shuai HUANG1,2,3, Jianhui GE1,2,3, Guangtao SONG1,2,3
Received:2024-08-21
Revised:2024-09-12
Accepted:2024-10-15
Online:2024-10-30
Published:2024-10-29
Contact:
Jinglei XU
E-mail:xujl@nuaa.edu.cn
Supported by:CLC Number:
Lixiang WEI, Jinglei XU, Kuangshi CHEN, Shuai HUANG, Jianhui GE, Guangtao SONG. Scheme design and performance study of adjustable vector nozzle for wide-range hypersonic aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2025, 46(8): 631086.
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