航空航天工程
空气动力学
弹道
攻角
解算器
翼
飞机飞行力学
俯仰角
计算机科学
机制(生物学)
航空学
模拟
工程类
物理
量子力学
天文
地球物理学
程序设计语言
作者
Andreas Goerttler,Christian Schnepf
出处
期刊:Journal of Aircraft
[American Institute of Aeronautics and Astronautics]
日期:2023-11-07
卷期号:: 1-14
摘要
Launching a fixed-wing unmanned aerial vehicle (UAV) out of the cargo hold of a flying transport aircraft (TA) is numerically investigated. A numerical tool chain is established to capture the dynamic motion of the UAV during launch, in which the DLR-TAU Code flow solver is coupled with a flight mechanics tool. A parameter study investigates how the UAV launch speed, position, and orientation relative to the loading platform of two different TAs affect its trajectory and aerodynamic behaviors. Furthermore, the influence of the angle of attack of the TA on the UAV trajectory and pitch angle is analyzed. This information will help design a launch mechanism that ensures a safe separation and aerodynamically stable flight after launch.
科研通智能强力驱动
Strongly Powered by AbleSci AI