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International Journal of Aerospace Engineering
Volume 2017 (2017), Article ID 1874729, 15 pages
https://doi.org/10.1155/2017/1874729
Research Article

Three-Dimensional CST Parameterization Method Applied in Aircraft Aeroelastic Analysis

Shaanxi Aerospace Flight Vehicle Design Key Laboratory, Northwestern Polytechnical University, Xi’an, Shaanxi 710072, China

Correspondence should be addressed to Hua Su; nc.ude.upwn@us

Received 3 March 2017; Accepted 18 June 2017; Published 4 October 2017

Academic Editor: Kenneth M. Sobel

Copyright © 2017 Hua Su 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.

How to Cite this Article

Hua Su, Chunlin Gong, and Liangxian Gu, “Three-Dimensional CST Parameterization Method Applied in Aircraft Aeroelastic Analysis,” International Journal of Aerospace Engineering, vol. 2017, Article ID 1874729, 15 pages, 2017. doi:10.1155/2017/1874729