書誌事項
- タイトル別名
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- 0703 Effect of center of flapping amplitude for flapping flight without tail-plane
抄録
In this study,it is clarified effect of center of flapping amplitude(CFA) for body angle on flapping flight without tail-plane.The average of body angle has negative correlation to CFA on flight of a flapping robot and two butterflies from results of observations for these flights.From this result,CFA is one of important factor for flapping flight.By using an equation of moment around flapping robot,it is considered that the body angle change is occurred by translation of application point of aerodynamic force due to CFA change.Moreover,the moment variation on CFA changing depends on point and direction of application of aerodynamic force and angle of attack.
収録刊行物
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- 流体工学部門講演会講演論文集
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流体工学部門講演会講演論文集 2012 (0), 281-282, 2012
一般社団法人 日本機械学会
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詳細情報 詳細情報について
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- CRID
- 1390282680860669952
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- NII論文ID
- 110009951687
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- ISSN
- 24242896
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- 本文言語コード
- ja
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- データソース種別
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- JaLC
- Crossref
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可