Table of Contents Author Guidelines Submit a Manuscript
Modelling and Simulation in Engineering
Volume 2011, Article ID 293078, 13 pages
http://dx.doi.org/10.1155/2011/293078
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.

Linked References

  1. M. Fujino and Y. Kawamura, “Wave-drag characteristics of an over-the-wing nacelle business-jet configuration,” Journal of Aircraft, vol. 40, no. 6, pp. 1177–1184, 2003. View at Google Scholar · View at Scopus
  2. J. Ricouard, R. Davy, P. Loheac, A. Moore, and O. Piccin, “ROSAS wind tunnel test campaign dedicated to unconventional aircraft concepts study,” in Proceedings of the 10th AIAA/CEAS Aeroacoustics Conference, pp. 783–792, Manchester, UK, May 2004. View at Scopus
  3. D. Sasaki and S. Obayashi, “Efficient search for trade-offs by adaptive range multi-objective genetic algorithms,” Journal of Aerospace Computing, Information and Communication, vol. 2, no. 1, pp. 44–64, 2005. View at Google Scholar · View at Scopus
  4. M. Sunago, D. Sasaki, K. Takenaka, and K. Nakahashi, “Multipoint optimization of a short-range quiet passenger aircraft,” Journal of Aircraft, vol. 46, no. 3, pp. 1070–1074, 2009. View at Publisher · View at Google Scholar · View at Scopus
  5. S. Jeong, Y. Minemura, and S. Obayashi, “Optimization of combustion chamber for diesel engine using kriging model,” Journal of Fluid Science and Technology, vol. 1, pp. 138–146, 2006. View at Google Scholar
  6. S. Jeong, M. Murayama, and K. Yamamoto, “Efficient optimization design method using kriging model,” Journal of Aircraft, vol. 42, no. 2, pp. 413–420, 2005. View at Google Scholar · View at Scopus
  7. M. D. McKay, R. J. Beckman, and W. J. Conover, “A comparison of three methods for selecting values of input variables in the analysis of output from a computer code,” Technometrics, vol. 21, no. 2, pp. 239–245, 1979. View at Google Scholar · View at Scopus
  8. November 2010, http://aaac.larc.nasa.gov/tsab/cfdlarc/aiaa-dpw/Workshop3/DPW3-geom.html.
  9. H. Sobieczky, “Parametric airfoils and wings,” in Notes on Numerical Fluid Mechanics, pp. 71–88, 1998. View at Google Scholar
  10. Y. Ito and K. Nakahashi, “Surface triangulation for polygonal models based on CAD data,” International Journal for Numerical Methods in Fluids, vol. 39, no. 1, pp. 75–96, 2002. View at Publisher · View at Google Scholar · View at Scopus
  11. D. Sharov and K. Nakahashi, “Hybrid prismatic/tetrahedral grid generation for viscous flow applications,” AIAA Journal, vol. 36, no. 2, pp. 157–162, 1998. View at Google Scholar · View at Scopus
  12. K. Nakahashi, Y. Ito, and F. Togashi, “Some challenges of realistic flow simulations by unstructured grid CFD,” International Journal for Numerical Methods in Fluids, vol. 43, no. 6-7, pp. 769–783, 2003. View at Google Scholar · View at Scopus
  13. S. Obayashi and G. P. Guruswamy, “Convergence acceleration of a Navier-Stokes solver for efficient static aeroelastic computations,” AIAA journal, vol. 33, no. 6, pp. 1134–1141, 1995. View at Google Scholar · View at Scopus
  14. V. Venkatakrishnan, “On the accuracy of limiters and convergence to steady-state solutions,” AIAA Paper 93-0880, 1992. View at Google Scholar
  15. D. Sharov and K. Nakahashi, “Reordering of hybrid unstructured grids for lower-upper symmetric Gauss-Seidel computations,” AIAA Journal, vol. 36, no. 3, pp. 484–486, 1998. View at Google Scholar · View at Scopus