Published January 6, 2015
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Figure 14 in Computational investigation of cicada aerodynamics in forward flight
Authors/Creators
- 1. Aerospace Systems Directorate, Air Force Research Laboratory, WPAFB, OH 45433, USA
- 2. Department of Mechanical and Aerospace Engineering, University of Virginia, Charlottesville, VA 22904, USA
- 3. Department of Mechanical and Materials Engineering, Wright State University, Dayton, OH 45435, USA
Description
Figure 14. Vortex structure at the end of downstroke (coloured by unified spanwise vorticity, colour max/min ¼ ±4). (Online version in colour.)
Notes
Published as part of Wan, Hui, Dong, Haibo & Gai, Kuo, 2015, Computational investigation of cicada aerodynamics in forward flight, pp. 1-14 in Journal of The Royal Society Interface 12 (102) on page 11, DOI: 10.1098/rsif.2014.1116, http://zenodo.org/record/10084618
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- Is part of
- Journal article: 10.1098/rsif.2014.1116 (DOI)
- Journal article: urn:lsid:plazi.org:pub:FFBFFFB3FFD0FC69FFCA09535A55FE68 (LSID)
- Journal article: https://zenodo.org/record/10084618 (URL)