跳到主要导航 跳到搜索 跳到主要内容

Study of airship stability based on a low resistance profile

  • Beihang University

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

Numerical simulation was conducted to investigate the external flow around airships with different tail layout, with the help of FLUENT 14.5, based on the incompressible Navier-Stokes equation and SST k -ω turbulent model. The aerodynamic information of the airships with different tail layout, such as pressure coefficient, torque coefficient and pressure distribution, were analyzed, and the numerical results showed the details of the airship surface flow and changes with different attack angle. According to the results, different tail layout had important influences on the aerodynamics and stability of airship. This will help to understand the aerodynamic characters around the tails of the stratospheric airship, and provide a reference in choosing tail layouts and the stability design of airships.

源语言英语
主期刊名Chemical and Mechanical Engineering, Information Technologies
1493-1496
页数4
DOI
出版状态已出版 - 2013
活动2013 3rd International Symposium on Chemical Engineering and Material Properties, ISCEMP 2013 - Sanya, 中国
期限: 22 6月 201324 6月 2013

出版系列

姓名Advanced Materials Research
791
ISSN(印刷版)1022-6680

会议

会议2013 3rd International Symposium on Chemical Engineering and Material Properties, ISCEMP 2013
国家/地区中国
Sanya
时期22/06/1324/06/13

指纹

探究 'Study of airship stability based on a low resistance profile' 的科研主题。它们共同构成独一无二的指纹。

引用此