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International Journal of Aerospace Engineering
Volume 2015, Article ID 956317, 8 pages
http://dx.doi.org/10.1155/2015/956317
Research Article

Investigation of Flow Control for the Hypersonic Inlets via Counter Flow

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

Received 1 April 2015; Accepted 4 June 2015

Academic Editor: Linda L. Vahala

Copyright © 2015 Xiaoqiang Fan and Yuan Tao. 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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