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Wing aeroelasticity analysis based on an integral boundary-layer method coupled with Euler solver

Crossref DOI link: https://doi.org/10.1016/j.cja.2016.08.013

Published Print: 2016-10

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Authors

Ma, Yanfeng

He, Erming

Zeng, Xianang

Li, Junjie
Funding

Funding for this research was provided by:

National Natural Science Foundation of China (51675426)

Aerospace Science and Technology Innovation Fund of China (2014KC010043)
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Text and Data Mining valid from 2016-10-01

Text and Data Mining valid from 2016-10-01

Version of Record valid from 2016-08-23
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This article is maintained by: Elsevier

Article Title: Wing aeroelasticity analysis based on an integral boundary-layer method coupled with Euler solver

Journal Title: Chinese Journal of Aeronautics

CrossRef DOI link to publisher maintained version: https://doi.org/10.1016/j.cja.2016.08.013

Content Type: article

Copyright: © 2016 Production and hosting by Elsevier Ltd. on behalf of Chinese Society of Aeronautics and Astronautics.