Correction to: Adv Aerodyn (2020) 2:5
https://doi.org/10.1186/s42774-020-0029-0
Following publication of the original article [1], the authors identified errors in Figs. 2 and 7. The correct figures are given below.
Experimental apparatus and model (a) the fast lift measurement platform, (b) experimental test model, (c) Wing structure, (d) the flapping wings with clap-and-fling motion
Aerodynamics, pressure distribution and flow field of the flapping wing with or without clap-and-fling effect in typical time. a-c lift, drag, aerodynamic power coefficient changes during a stroke cycle, d pressure distribution of typical time
Reference
Cheng C, Wu J, Zhang Y et al (2020) Aerodynamics and dynamic stability of micro-air-vehicle with four flapping wings in hovering flight. Adv Aerodyn 2:5 https://doi.org/10.1186/s42774-020-0029-0
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Cheng, C., Wu, J., Zhang, Y. et al. Correction to: Aerodynamics and dynamic stability of micro-air-vehicle with four flapping wings in hovering flight. Adv. Aerodyn. 2, 16 (2020). https://doi.org/10.1186/s42774-020-00040-z
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DOI: https://doi.org/10.1186/s42774-020-00040-z