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起落架舱对运输类飞机机身阻力特性的影响研究
引用本文:郑隆乾,杨永. 起落架舱对运输类飞机机身阻力特性的影响研究[J]. 航空计算技术, 2010, 40(4): 56-58
作者姓名:郑隆乾  杨永
作者单位:西北工业大学,航空学院,陕西,西安,710072;西北工业大学,航空学院,陕西,西安,710072
摘    要:通过对后体上翘的运输类飞机机身(机身+起落架舱)的CFD数值模拟,研究了起落架舱对机身最小阻力攻角的影响。结果表明:对于后体上翘较大的运输类飞机,相对于净机身,加上起落架舱后,机身阻力增加,但最小阻力攻角明显减小。

关 键 词:上翘后体  起落架舱  小阻力  攻角  CFD  数值模拟

Influence of Landing Gear Cabin on Drag of a Transport Aircraft Body
ZHENG Long-qian,YANG Yong. Influence of Landing Gear Cabin on Drag of a Transport Aircraft Body[J]. Aeronautical Computer Technique, 2010, 40(4): 56-58
Authors:ZHENG Long-qian  YANG Yong
Affiliation:(School of Aeronautics,Northwestern Polytechnical University,Xi′an 710072,China)
Abstract:A computational investigation of the impact of landing gear cabin on drag has been conducted.Numerical simulations on fuselage of transport airplane with/without landing gear cabin were taken by solving RANS equations with SA turbulence model.The primary emphasis in this paper is on fuselage with afterbody of 17°upswept angle.The comparison shows that drag increases,but the attack angle of minimal drag is obviously decreased on fuselage with landing gear cabin.
Keywords:CFD
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