高超声速翼舵干扰气动特性研究综述
发布时间：2019-06-28 16:31
【摘要】：有翼高超声速飞行器已取得了较为广泛的应用,有翼高超声速飞行器复杂翼舵干扰对飞行器气动特性有很大的影响。半个世纪以来,高超声速翼舵干扰集中在鸭翼与主翼的气动干扰研究,而针对主翼与全动舵气动干扰的研究较少。对主翼与舵干扰、鸭翼与主翼干扰气动特性研究现状进行了概述,并对翼舵干扰的关键问题进行了总结。
[Abstract]:The winged hypersonic vehicle has been widely used. The complex wing rudder interference of the winged hypersonic vehicle has a great influence on the aerodynamic characteristics of the aircraft. For half a century, hypersonic wing rudder interference has focused on the pneumatic interference between duck wing and main wing, while the research on main wing and fully moving rudder has been less. The research status of main wing and rudder interference, duck wing and main wing interference is summarized, and the key problems of wing and rudder interference are summarized.
【作者单位】： 北京航空航天大学;
【分类号】：TJ760;V211
，
本文编号：2507447
[Abstract]:The winged hypersonic vehicle has been widely used. The complex wing rudder interference of the winged hypersonic vehicle has a great influence on the aerodynamic characteristics of the aircraft. For half a century, hypersonic wing rudder interference has focused on the pneumatic interference between duck wing and main wing, while the research on main wing and fully moving rudder has been less. The research status of main wing and rudder interference, duck wing and main wing interference is summarized, and the key problems of wing and rudder interference are summarized.
【作者单位】： 北京航空航天大学;
【分类号】：TJ760;V211
，
本文编号：2507447
本文链接：https://www.wllwen.com/kejilunwen/hangkongsky/2507447.html
