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Inverse optimization method for blunt-trailing-edge airfoils

  • Shigeru Obayashi
  • Shinkyu Jeong
  • Yuichi Matsuo
Algorithms Numerical Techniques
Part of the Lecture Notes in Physics book series (LNP, volume 490)

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References

  1. 1.
    Obayashi, S. and Takanashi, S., “Genetic Optimization of Target Pressure Distributions for Inverse Design Methods,” AIAA Journal Vol. 34 No. 5, May 1996, pp. 881–886.CrossRefADSGoogle Scholar
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    Henne, P. A., “Innovation with Computational Aerodynamics: The Divergent Trailing-Edge Airfoil,” Applied Computational Aerodynamics, Seebass (ed.), Progress in Astronautics and Aeronautics, Vol. 125, AIAA, Washington D. C., 1990, pp. 221–262.Google Scholar
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    Matsuo, Y., and Chyu, W. J., “Computation of Separated Flows Using a Low Reynolds Number k-ε Model,” Proceedings of the 5th International Symposium on Computational Fluid Dynamics, Sendai, Vol. II, 1993, pp. 206–211.Google Scholar
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    Stanaway, S. K., McCroskey, W. J. and Kroo, I. M., “Navier-Stokes Analysis of Blunt Trailing Edge Airfoils,” AIAA Paper 92-0024, Reno, Nevada, Jan. 1992.Google Scholar
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    Monsen, E. and Rudnik, R., “Investigation of the Blunt Trailing Edge Problem for Supercritical Airfoils,” AIAA Paper 95-0089, Reno, Nevada, Jan. 1995.Google Scholar
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    Takanashi, S., “Iterative Three-Dimensional Transonic Wing Design Using Integral Equations,” Journal of Aircraft, Vol. 22, No. 8, August 1985, pp. 655–660.CrossRefGoogle Scholar
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    Harris, C. D., “NASA Supercritical Airfoils — A Matrix of Family-Related Airfoils,” NASA TP-2969, March 1990.Google Scholar

Copyright information

© Springer-Verlag 1997

Authors and Affiliations

  • Shigeru Obayashi
    • 1
  • Shinkyu Jeong
    • 1
  • Yuichi Matsuo
    • 2
  1. 1.Tohoku UniversitySendaiJapan
  2. 2.National Aerospace LaboratoryChofuJapan

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