中国航空学报（英文版）2026，Vol.39Issue(1)：66-77,12.DOI:10.1016/j.cja.2025.103582
Yaw stabilization and maneuvering control of tailless flying wing by co-directional fluidic thrust vectoring
Yaw stabilization and maneuvering control of tailless flying wing by co-directional fluidic thrust vectoring
Liu ZHANG 1Meng HE2
作者信息
- 1. State Key Laboratory of Aerodynamics,China Aerodynamics Research and Development Center,Mianyang 621000,China
- 2. Low Speed Aerodynamics Institute,China Aerodynamics Research and Development Center,Mianyang 621000,China
- 折叠
摘要
关键词
Thrust vectoring/Flow control/Coanda effect/Flying-wing aircraft/Flight tests/Yaw controlKey words
Thrust vectoring/Flow control/Coanda effect/Flying-wing aircraft/Flight tests/Yaw control引用本文复制引用
Liu ZHANG,Meng HE..Yaw stabilization and maneuvering control of tailless flying wing by co-directional fluidic thrust vectoring[J].中国航空学报（英文版）,2026,39(1):66-77,12.
