Erratum to: Ornithopter flight simulation based on flexible multi-body dynamics

被引:0
|
作者
Andreas T. Pfeiffer
Jun-Seong Lee
Jae-Hung Han
Horst Baier
机构
[1] KAIST,Department of Aerospace Engineering
[2] Technical University Munich,The Institute of Lightweight Structures, Aerospace Department
来源
关键词
ornithopter; flexible multi-body dynamics; flight stability; trim flight;
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暂无
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学科分类号
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]
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页码:209 / 209
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