When static directional stability of an aircraft is unstable,the typical effectiveness of the vertical tail and rudder to the yawing moment falls off because the vertical tail gradually becomes enveloped in the wake of wing and fuselage. Meanwhile,the forebody remains in the undisturbed flow field,and therefore the static directional stability can be enhanced though addition of forebody strake at the forebody. From the results of a series of experiments on forebody strake,it was found that the angle of atta...
【基金】
国家自然科学基金(11272035)~~
【更新日期】
2016-11-01
【分类号】
V212.13
【正文快照】
网络出版地址:www.cnki.net/kcms/detail/11.2625.V.20160324.0919.002.html引用格式:闻静,王延奎,邓学蓥.前体边条控制技术对航向静稳定性的影响[J].北京航空航天大学学报,2016,42(10):2180-2188.WEN J,WANG Y K,DENG X Y.Effect of forebody strake control technology on st
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