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Modelling and Simulation in Engineering
Volume 2011, Article ID 293078, 13 pages
Research Article

Aerodynamic Optimization of an Over-the-Wing-Nacelle-Mount Configuration

Department of Aerospace Engineering, Tohoku University, Aoba 6-6-01, Sendai 980-8579, Japan

Received 14 November 2010; Revised 21 February 2011; Accepted 21 February 2011

Academic Editor: Guan Yeoh

Copyright © 2011 Daisuke Sasaki and Kazuhiro Nakahashi. 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 [1 citation]

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

  • Yuma Fukushima, Daisuke Sasaki, and Kazuhiro Nakahashi, “Cartesian Mesh Linearized Euler Equations Solver for Aeroacoustic Problems around Full Aircraft,” International Journal of Aerospace Engineering, vol. 2015, pp. 1–18, 2015. View at Publisher ยท View at Google Scholar