CIOMP OpenIR
Numerical investigation on buffeting and lock-in phenomenon for biplane airfoils at alpha=40 degrees
R. Guo; Y. Bai; Z. Qiao; X. Pei and G. Wu
2022
发表期刊International Journal of Mechanical Sciences
ISSN207403
卷号219
摘要Biplane airfoils at high angles of attack have interesting nonlinear characteristics, the purpose of this work is to evaluate the impacts of spacing ratio (=ds/c=0.25, 0.5, 1, 2 and 4, where ds is the vertical distance between biplane airfoils and c is chord length) and Reynolds number (0.87105Re4.35105) on buffeting and lock-in phenomenon at angle of attack =40 throughout numerical investigation. Present simulation results show that biplane configuration usually can reduce buffeting frequency slightly comparing to the single airfoil, yet reasonable spacing =2 is helpful to suppress buffeting and continuous acceleration also promotes stability. Particular attention is paid to stagnation point region that moves away from leading edge of the upper airfoil with increasing . However, the lower airfoil corresponds to the fixed stagnation point region. Additionally, limit cycle oscillation (LCO) of biplane airfoils is determined by pitching angles (), and in consideration of spacing effect, limit cycles of the lower airfoil move downward but those of the upper airfoil move in the opposite direction. Moreover, the shape of limit cycle for the later first collapses then inflates. Unique 8-shaped hysteresis of the upper airfoil in =1 is caused by sporadically wake interference. On the whole, V-shaped lock-in region will expand and shift left to some extent based on in contrast to the single airfoil. In terms of area, lock-in region shrinks then expands with rising , and the proportion of the left part increases as increases. 2022 Elsevier Ltd
DOI10.1016/j.ijmecsci.2022.107120
URL查看原文
收录类别ei
引用统计
文献类型期刊论文
条目标识符http://ir.ciomp.ac.cn/handle/181722/67264
专题中国科学院长春光学精密机械与物理研究所
推荐引用方式
GB/T 7714
R. Guo,Y. Bai,Z. Qiao,et al. Numerical investigation on buffeting and lock-in phenomenon for biplane airfoils at alpha=40 degrees[J]. International Journal of Mechanical Sciences,2022,219.
APA R. Guo,Y. Bai,Z. Qiao,&X. Pei and G. Wu.(2022).Numerical investigation on buffeting and lock-in phenomenon for biplane airfoils at alpha=40 degrees.International Journal of Mechanical Sciences,219.
MLA R. Guo,et al."Numerical investigation on buffeting and lock-in phenomenon for biplane airfoils at alpha=40 degrees".International Journal of Mechanical Sciences 219(2022).
条目包含的文件 下载所有文件
文件名称/大小 文献类型 版本类型 开放类型 使用许可
Numerical investigat(5806KB)期刊论文出版稿开放获取CC BY-NC-SA浏览 下载
个性服务
推荐该条目
保存到收藏夹
查看访问统计
导出为Endnote文件
谷歌学术
谷歌学术中相似的文章
[R. Guo]的文章
[Y. Bai]的文章
[Z. Qiao]的文章
百度学术
百度学术中相似的文章
[R. Guo]的文章
[Y. Bai]的文章
[Z. Qiao]的文章
必应学术
必应学术中相似的文章
[R. Guo]的文章
[Y. Bai]的文章
[Z. Qiao]的文章
相关权益政策
暂无数据
收藏/分享
文件名: Numerical investigation on buffeting and lock-.pdf
格式: Adobe PDF
所有评论 (0)
暂无评论
 

除非特别说明,本系统中所有内容都受版权保护,并保留所有权利。