首页 | 本学科首页   官方微博 | 高级检索  
     

斜置飞翼翼型气动性能的研究
引用本文:冯军红,赵亮. 斜置飞翼翼型气动性能的研究[J]. 科技信息, 2011, 0(13): 451-452
作者姓名:冯军红  赵亮
作者单位:中国民航飞行学院,四川广汉618307
摘    要:斜置飞翼是一种具有亚音速和超声速巡航能力的可变后掠角飞机。本文根据斜置飞翼的飞行特点和气动特性,选用了相对弯度、相对厚度等参数不同的两种翼型。通过数值模拟分析,对比两种翼型在不同迎角和雷诺数下的空气动力性能,结果表明翼型2的气动性能优于翼型1。

关 键 词:斜置飞翼  翼型  升阻比

Research on the Aerodynamic Performance of OFW Airfoil
FENG Jun-hong,ZHAO Liang. Research on the Aerodynamic Performance of OFW Airfoil[J]. Science, 2011, 0(13): 451-452
Authors:FENG Jun-hong  ZHAO Liang
Affiliation:(Civil Aviation Flight University of China, Guanghan Sichuan, 618307,China)
Abstract:Oblique flying wing with subsonic and supersonic cruising ability of variable sweep aircraft.According to the characteristics and aerodynamic properties of oblique llying wing, selected two different kinds of te airfoil with relalive camber, relative thickness of parameters. Based on rmmerical simulation, in comparison to the two airfoil aerodynamics at different angles of attack and Reynolds number, the resuhs show that the wing Type 2 airfoil aerodynamic performance is better than type I.
Keywords:Oblique flying wing  Airfbil: Lift-drag ratio
本文献已被 CNKI 维普 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号