Aerodynamic characteristics of hoverflies during hovering flight
The aerodynamic characteristics of model hoverflies during hovering flight are studied with a three-dimensional sharp-interface immersed boundary method. The wing is modelled as a rectangular generic wing to test the effects of an accessory flap called the alula, which is located at the wing root. S...
主要な著者: | Tian, F, Tobing, S, Young, J, Lai, J, Walker, S, Taylor, G, Thomas, A |
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フォーマット: | Journal article |
出版事項: |
Elsevier
2018
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