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International Journal of Aerospace Engineering
Volume 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.

Citations to this Article [7 citations]

The following is the list of published articles that have cited the current article.

  • Vijay Kumar Patidar, Rajesh Yadav, and Sudhir Joshi, “Numerical investigation of the effect of stagger on the aerodynamic characteristics of a Busemann biplane,” Aerospace Science and Technology, 2016. View at Publisher · View at Google Scholar
  • A. Kuzmin, “Shock wave bifurcation in convergent–divergent channels of rectangular cross section,” Shock Waves, 2016. View at Publisher · View at Google Scholar
  • Shuhan Liu, and Zhanxia Zhu, “Aerodynamic characteristics of hypersonic morphing biplane,” Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, vol. 38, no. 9, 2017. View at Publisher · View at Google Scholar
  • Alexander Kuzmin, “Transonic flow instability in the entrance region of a channel with breaks of walls,” Archive of Applied Mechanics, 2017. View at Publisher · View at Google Scholar
  • Zvegintsev, “Gas-dynamic problems in off-design operation of supersonic inlets (review),” Thermophysics and Aeromechanics, vol. 24, no. 6, pp. 807–834, 2017. View at Publisher · View at Google Scholar
  • A. Kuzmin, “Transonic flow hysteresis in a twin intake model,” The Aeronautical Journal, vol. 122, no. 1256, pp. 1557–1567, 2018. View at Publisher · View at Google Scholar
  • Seong-kyun Im, and Hyungrok Do, “Unstart phenomena induced by flow choking in scramjet inlet-isolators,” Progress in Aerospace Sciences, 2018. View at Publisher · View at Google Scholar