International Journal of Aerospace Engineering

International Journal of Aerospace Engineering / 2020 / Article

Corrigendum | Open Access

Volume 2020 |Article ID 2825862 | https://doi.org/10.1155/2020/2825862

Haoying Chen, Haibo Zhang, Zhihua Xi, Qiangang Zheng, "Corrigendum to “Study on Inlet and Engine Integrated Model with Normal Shock Position Feedback”", International Journal of Aerospace Engineering, vol. 2020, Article ID 2825862, 1 page, 2020. https://doi.org/10.1155/2020/2825862

Corrigendum to “Study on Inlet and Engine Integrated Model with Normal Shock Position Feedback”

Received18 Nov 2020
Accepted18 Nov 2020
Published07 Dec 2020

In the article titled “Study on Inlet and Engine Integrated Model with Normal Shock Position Feedback” [1], there was an error in the Acknowledgments section. The corrected section appears below:

Acknowledgments

This study is supported in part by the National Science and Technology Major Project under Grant 2017-V-0004-0054, Research on the Basic Problem of Intelligent Aero-engine under Grant 2017-JCJQ-ZD-047-21, National Natural Science Foundation of China under Grant 51906102, China Postdoctoral Science Foundation Funded Project under Grant 2019M661835, and Aeronautics Power Foundation under Grant 6141B09050385.

References

  1. H. Chen, H. Zhang, Z. Xi, and Q. Zheng, “Study on inlet and engine integrated model with normal shock position feedback,” International Journal of Aerospace Engineering, vol. 2020, Article ID 5313941, 13 pages, 2020. View at: Publisher Site | Google Scholar

Copyright © 2020 Haoying Chen et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.


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