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International Journal of Aerospace Engineering
Volume 2013 (2013), Article ID 231434, 10 pages
http://dx.doi.org/10.1155/2013/231434
Research Article

Wind Tunnel Testing on Start/Unstart Characteristics of Finite Supersonic Biplane Wing

1Institute of Fluid Science, Tohoku University, Sendai 980-8577, Japan
2Institut für Physik der Atmosphäre, Deutsches Zentrum für Luft- und Raumfahrt, 82234 Oberpfaffenhofen, Germany
3Honda R&D Co., Ltd., Haga 321-3321, Japan
4Department of Aerospace Engineering, Tohoku University, Sendai 980-8579, Japan

Received 17 July 2013; Accepted 20 September 2013

Academic Editor: James J. McGuirk

Copyright © 2013 Hiroshi Yamashita 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

Hiroshi Yamashita, Naoshi Kuratani, Masahito Yonezawa, et al., “Wind Tunnel Testing on Start/Unstart Characteristics of Finite Supersonic Biplane Wing,” International Journal of Aerospace Engineering, vol. 2013, Article ID 231434, 10 pages, 2013. doi:10.1155/2013/231434