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

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

Bibliographic Details
Main Authors: Haoying Chen, Haibo Zhang, Zhihua Xi, Qiangang Zheng
Format: Article
Language:English
Published: Hindawi Limited 2020-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2020/2825862
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spelling doaj-dbfde6c980424081bb540f88c13ec5f22020-12-21T11:41:30ZengHindawi LimitedInternational Journal of Aerospace Engineering1687-59661687-59742020-01-01202010.1155/2020/28258622825862Corrigendum to “Study on Inlet and Engine Integrated Model with Normal Shock Position Feedback”Haoying Chen0Haibo Zhang1Zhihua Xi2Qiangang Zheng3Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, No. 29 Yudao Street, Nanjing 210016, ChinaJiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, No. 29 Yudao Street, Nanjing 210016, ChinaJiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, No. 29 Yudao Street, Nanjing 210016, ChinaJiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, No. 29 Yudao Street, Nanjing 210016, Chinahttp://dx.doi.org/10.1155/2020/2825862
collection DOAJ
language English
format Article
sources DOAJ
author Haoying Chen
Haibo Zhang
Zhihua Xi
Qiangang Zheng
spellingShingle 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
author_facet Haoying Chen
Haibo Zhang
Zhihua Xi
Qiangang Zheng
author_sort Haoying Chen
title Corrigendum to “Study on Inlet and Engine Integrated Model with Normal Shock Position Feedback”
title_short Corrigendum to “Study on Inlet and Engine Integrated Model with Normal Shock Position Feedback”
title_full Corrigendum to “Study on Inlet and Engine Integrated Model with Normal Shock Position Feedback”
title_fullStr Corrigendum to “Study on Inlet and Engine Integrated Model with Normal Shock Position Feedback”
title_full_unstemmed Corrigendum to “Study on Inlet and Engine Integrated Model with Normal Shock Position Feedback”
title_sort corrigendum to “study on inlet and engine integrated model with normal shock position feedback”
publisher Hindawi Limited
series International Journal of Aerospace Engineering
issn 1687-5966
1687-5974
publishDate 2020-01-01
url http://dx.doi.org/10.1155/2020/2825862
work_keys_str_mv AT haoyingchen corrigendumtostudyoninletandengineintegratedmodelwithnormalshockpositionfeedback
AT haibozhang corrigendumtostudyoninletandengineintegratedmodelwithnormalshockpositionfeedback
AT zhihuaxi corrigendumtostudyoninletandengineintegratedmodelwithnormalshockpositionfeedback
AT qiangangzheng corrigendumtostudyoninletandengineintegratedmodelwithnormalshockpositionfeedback
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