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International Journal of Aerospace Engineering
Volume 2015, Article ID 672423, 22 pages
http://dx.doi.org/10.1155/2015/672423
Review Article

A Review of Wind Tunnel Based Virtual Flight Testing Techniques for Evaluation of Flight Control Systems

Science and Technology on Scramjet Laboratory, National University of Defense Technology, Changsha, Hunan 410073, China

Received 8 June 2015; Revised 30 August 2015; Accepted 18 October 2015

Academic Editor: Paolo Tortora

Copyright © 2015 Min Huang and Zhong-wei Wang. 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

Min Huang and Zhong-wei Wang, “A Review of Wind Tunnel Based Virtual Flight Testing Techniques for Evaluation of Flight Control Systems,” International Journal of Aerospace Engineering, vol. 2015, Article ID 672423, 22 pages, 2015. https://doi.org/10.1155/2015/672423.