Computational investigation of cicada aerodynamics in forward flight |
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| Authors: | Hui Wan Haibo Dong Kuo Gai |
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| Affiliation: | 1Aerospace Systems Directorate, Air Force Research Laboratory, WPAFB, OH 45433, USA;2Department of Mechanical and Aerospace Engineering, University of Virginia, Charlottesville, VA 22904, USA;3Department of Mechanical and Materials Engineering, Wright State University, Dayton, OH 45435, USA |
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| Abstract: | Free forward flight of cicadas is investigated through high-speed photogrammetry, three-dimensional surface reconstruction and computational fluid dynamics simulations. We report two new vortices generated by the cicada''s wide body. One is the thorax-generated vortex, which helps the downwash flow, indicating a new phenomenon of lift enhancement. Another is the cicada posterior body vortex, which entangles with the vortex ring composed of wing tip, trailing edge and wing root vortices. Some other vortex features include: independently developed left- and right-hand side leading edge vortex (LEV), dual-core LEV structure at the mid-wing region and near-wake two-vortex-ring structure. In the cicada forward flight, approximately 79% of the total lift is generated during the downstroke. Cicada wings experience drag in the downstroke, and generate thrust during the upstroke. Energetics study shows that the cicada in free forward flight consumes much more power in the downstroke than in the upstroke, to provide enough lift to support the weight and to overcome drag to move forward. |
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| Keywords: | insect free flight insect aerodynamics low Reynolds number flow |
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