Experimental study on flow interaction between fore- and hindwings of dragnofly in hovering and forward flight

Hiroto Nagai, Koji Isogai, Tatsumi Fujimoto

研究成果: 著書/レポートタイプへの貢献会議での発言

8 引用 (Scopus)

抄録

There are various flow interactions between the fore- and hindwings of a dragonfly. However, the detailed mechanism of flow interaction between the fore- and hindwings has not been well understood. In this study, we clarify the aerodynamic mechanisms of flow interaction between fore- and hindwings of a dragonfly in hovering and forward flights. Measurements of unsteady aerodynamic forces acting on the tandem wings are conducted using a dynamically scaled mechanical model in a water tunnel. Moreover, flow visualization around the tandem wings is conducted using Particle Image Velocimetry. The effect of the phase difference between the fore- and hindwings on the aerodynamic characteristics is investigated in hovering and forward flights. The results indicate that the advanced hindwing ahead of the forewing, which is often used in steady flights of dragonflies, has a smaller variation with respect to the phase difference and a smaller difference between the fore- and hindwings in hovering and forward flight. In hovering flight, the flow interaction reduces the aerodynamic characteristics except at the phase difference of 0 deg. In forward flight, the advanced hindwing generates larger lift with a good efficiency than that without interaction.

元の言語英語
ホスト出版物のタイトル27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010
ページ998-1007
ページ数10
出版物ステータス出版済み - 12 1 2010
イベント27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010 - Nice, フランス
継続期間: 9 19 20109 24 2010

出版物シリーズ

名前27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010
2

その他

その他27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010
フランス
Nice
期間9/19/109/24/10

Fingerprint

Flow interactions
Aerodynamics
Flow visualization
Velocity measurement
Wind tunnels
Water

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Control and Systems Engineering
  • Electrical and Electronic Engineering
  • Materials Science(all)

これを引用

Nagai, H., Isogai, K., & Fujimoto, T. (2010). Experimental study on flow interaction between fore- and hindwings of dragnofly in hovering and forward flight. : 27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010 (pp. 998-1007). (27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010; 巻数 2).

Experimental study on flow interaction between fore- and hindwings of dragnofly in hovering and forward flight. / Nagai, Hiroto; Isogai, Koji; Fujimoto, Tatsumi.

27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010. 2010. p. 998-1007 (27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010; 巻 2).

研究成果: 著書/レポートタイプへの貢献会議での発言

Nagai, H, Isogai, K & Fujimoto, T 2010, Experimental study on flow interaction between fore- and hindwings of dragnofly in hovering and forward flight. : 27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010. 27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010, 巻. 2, pp. 998-1007, 27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010, Nice, フランス, 9/19/10.
Nagai H, Isogai K, Fujimoto T. Experimental study on flow interaction between fore- and hindwings of dragnofly in hovering and forward flight. : 27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010. 2010. p. 998-1007. (27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010).
Nagai, Hiroto ; Isogai, Koji ; Fujimoto, Tatsumi. / Experimental study on flow interaction between fore- and hindwings of dragnofly in hovering and forward flight. 27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010. 2010. pp. 998-1007 (27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010).
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