Numerical simulation of loitering aircraft aerodynamics in low speed flight

Guanglin He*, Xiaolin Li

*此作品的通讯作者

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

Aerodynamic design rules of unconventional layout loitering aircraft against the issue of stall in low speed flight were proposed in this paper. Using the SST k-ω two equations turbulence model, the stalling characteristics of the loitering aircraft were studied. Based on the low speed flow field of the loitering aircraft without the deflexion of the helm, aerodynamic parameters such as lift, drag, pitching moment and yawing moment in different workings were calculated. Analysis of the results shows that the loitering aircraft designed has good stalling capability whose critical angle of attack is 18 degrees. The loitering aircraft has good longitudinal and lateral stability under different angle of attack.

源语言英语
主期刊名Advanced Research on Industry, Information System and Material Engineering
139-143
页数5
DOI
出版状态已出版 - 2011
活动2011 International Conference on Industry, Information System and Material Engineering, IISME2011 - Guangzhou, 中国
期限: 16 4月 201117 4月 2011

出版系列

姓名Advanced Materials Research
204-210
ISSN(印刷版)1022-6680

会议

会议2011 International Conference on Industry, Information System and Material Engineering, IISME2011
国家/地区中国
Guangzhou
时期16/04/1117/04/11

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