Skip to main content

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

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
figure1

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

Fig. 7
figure2

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

  1. 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

    Article  Google Scholar 

Download references

Author information

Affiliations

Authors

Corresponding author

Correspondence to Chao Zhou.

Rights and permissions

Open Access This article is licensed under a Creative Commons Attribution 4.0 International License, which permits use, sharing, adaptation, distribution and reproduction in any medium or format, as long as you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons licence, and indicate if changes were made. The images or other third party material in this article are included in the article's Creative Commons licence, unless indicated otherwise in a credit line to the material. If material is not included in the article's Creative Commons licence and your intended use is not permitted by statutory regulation or exceeds the permitted use, you will need to obtain permission directly from the copyright holder. To view a copy of this licence, visit http://creativecommons.org/licenses/by/4.0/.

Reprints and Permissions

About this article

Verify currency and authenticity via CrossMark

Cite this article

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

Download citation