Ornithopter flight simulation based on flexible multi-body dynamics (vol 7, pg 102, 2010)

被引:0
|
作者
Pfeiffer, A. T.
Lee, J. S.
Han, J. H.
Baier, H.
机构
[1] KAIST,Department of Aerospace Engineering
[2] Technical University Munich,The Institute of Lightweight Structures, Aerospace Department
关键词
ornithopter; flexible multi-body dynamics; flight stability; trim flight;
D O I
10.1016/S1672-6529(09)60209-2
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Due to our editing mistake, Fig. 9a in Ref. [1] was wrongly used. The correct Fig. 9 is given in the right. Fig. 9Coefficient of constraint forces and moment with respect to the flapping-wing motion (a), main-wing motion vs. the non-dimensional distance between χZMP and χCG for upstroke and downstroke motion (b). θMEAN = 9.2°, ƒ = 12 Hz, U = 10.8 m·s−1.[graphic not available: see fulltext]
引用
收藏
页码:209 / 209
页数:1
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