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Correction to: Aerodynamics and dynamic stability of micro-air-vehicle with four flapping wings in hovering flight

Advances in Aerodynamics volume 2, Article number: 16 (2020) Cite this article

The Original Article was published on 17 February 2020

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.

Fig. 2
figure 1

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

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Fig. 7
figure 2

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

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Reference

  1. 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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Authors and Affiliations

  1. School of Transportation Science and Engineering, Beihang University, Beijing, 100191, China

    Cheng Cheng, Jianghao Wu, Yanlai Zhang & Chao Zhou

  2. The first Aircraft Design Institute, Aviation Industry Coorporation of China, Xi’an, 710089, China

    Han Li

Authors
  1. Cheng Cheng
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  2. Jianghao Wu
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  3. Yanlai Zhang
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  4. Han Li
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  5. Chao Zhou
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Correspondence to Chao Zhou.

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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