Unsteady Thin-Airfoil Theory Revisited: Application of a Simple Lift Formula
文献类型:期刊论文
作者 | Liu TS; Wang SZ(王士召)![]() ![]() ![]() |
刊名 | AIAA Journal
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出版日期 | 2015-06 |
卷号 | 53期号:6页码:1492-1502 |
通讯作者邮箱 | tianshu.liu@wmich.edu |
ISSN号 | 0001-1452 |
产权排序 | [Liu, Tianshu] Western Michigan Univ, Dept Mech & Aerosp Engn, Kalamazoo, MI 49008 USA; [Wang, Shizhao; Zhang, Xing; He, Guowei] Chinese Acad Sci, Inst Mech, State Key Lab Nonlinear Mech, Beijing 100190, Peoples R China |
通讯作者 | Liu, TS (reprint author), Western Michigan Univ, Dept Mech & Aerosp Engn, Kalamazoo, MI 49008 USA. |
中文摘要 | The physical foundations of unsteady thin-airfoil theory are explored in the general framework of viscous flows. The thin-airfoil lift formula is derived by using the simple lift formula that contains the vortex lift and the lift associated with the fluid acceleration. From a broader perspective, the thin-airfoil lift formula could be applicable even when the flow around an airfoil is moderately separated, from which the classical von Karman-Sears lift formula can be recovered as a reduced case. The quantitative relationship between boundary layer and lift generation is discussed. Direct numerical simulations of low-Reynolds-number flows over a flapping flat-plate airfoil are conducted to examine the accuracy and limitations of the thin-airfoil lift formula. |
学科主题 | 力学 ; 流体力学 ; 空气动力学 |
分类号 | 一类 |
类目[WOS] | Engineering, Aerospace |
研究领域[WOS] | Engineering |
关键词[WOS] | FORCES ; FLOWS ; MOMENT ; MOTION |
收录类别 | SCI ; EI |
原文出处 | http://dx.doi.org/10.2514/1.J053439 |
语种 | 英语 |
WOS记录号 | WOS:000354386200008 |
源URL | [http://dspace.imech.ac.cn/handle/311007/58356] ![]() |
专题 | 力学研究所_非线性力学国家重点实验室 |
推荐引用方式 GB/T 7714 | Liu TS,Wang SZ,Zhang X,et al. Unsteady Thin-Airfoil Theory Revisited: Application of a Simple Lift Formula[J]. AIAA Journal,2015,53(6):1492-1502. |
APA | Liu TS,Wang SZ,Zhang X,&He GW.(2015).Unsteady Thin-Airfoil Theory Revisited: Application of a Simple Lift Formula.AIAA Journal,53(6),1492-1502. |
MLA | Liu TS,et al."Unsteady Thin-Airfoil Theory Revisited: Application of a Simple Lift Formula".AIAA Journal 53.6(2015):1492-1502. |
入库方式: OAI收割
来源:力学研究所
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