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- MAEDA Masateru
- Graduate School of Engineering, Chiba University
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- GAO Na
- Graduate School of Engineering, Chiba University
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- NISHIHASHI Naoshi
- Graduate School of Engineering, Chiba University
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- LIU Hao
- Graduate School of Engineering, Chiba University
説明
In insect flapping flight, non-equilibrium flight conditions such as takeoffs and uncoordinated turn are difficult to investigate with experiments or quasi-steady analysis. Here we develop a simplified rigid body dynamics solver with 6 degrees of freedom (DOF), by utilizing unit quaternions. A free-flight simulator of an insect flapping flight is then built up by coupling the dynamics solver with an in-house CFD solver, which is specified for simulating unsteady flapping-wing aerodynamics. Simulation of the hovering flight of a fruit fly (Drosophila melanogaster) is achieved by manually manipulating three kinematic parameters, wingbeat amplitude, mean positional angle, and stroke plane angle relative to body (anatomical stroke plane angle).
収録刊行物
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- Journal of Aero Aqua Bio-mechanisms
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Journal of Aero Aqua Bio-mechanisms 1 (1), 71-79, 2010
エアロ・アクアバイオメカニズム学会
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詳細情報 詳細情報について
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- CRID
- 1390001205342950912
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- NII論文ID
- 130000428321
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- ISSN
- 21851522
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- 本文言語コード
- en
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- データソース種別
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- JaLC
- Crossref
- CiNii Articles
- OpenAIRE
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- 抄録ライセンスフラグ
- 使用不可