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International Journal of Aerospace Engineering
Volume 2016 (2016), Article ID 3196057, 14 pages
http://dx.doi.org/10.1155/2016/3196057
Research Article

Receptivity of Boundary Layer over a Blunt Wedge due to Freestream Pulse Disturbances at Mach 6

1College of Aerospace and Civil Engineering, Harbin Engineering University, Harbin 150001, China
2Beijing Spacecrafts, China Academy of Space Technology, Beijing 100094, China

Received 23 July 2015; Revised 28 February 2016; Accepted 14 March 2016

Academic Editor: Saad A. Ahmed

Copyright © 2016 Jianqiang Shi 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.

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