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. 2013 Aug 6;10(85):20130312. doi: 10.1098/rsif.2013.0312

Figure 2.

Figure 2.

(a) Structured grid for Chimera mesh, (b) difference between rigid (skyblue) and flexible (red) hind wing models at typical time steps during downstroke and (c) kinematics of elytron and hind wing used in the simulation. (Online version in colour.)