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Aerodynamic Design of Wing-Engine Configuration under Effect of Jet Plume

  • Hitoshi Takahashi
  • Susumu Takanashi
  • Takuji Kishimoto
  • Kenji Hayama
  • Eiji Shima
Chapter
  • 310 Downloads
Part of the Notes on Numerical Fluid Mechanics (NNFM) book series (NONUFM, volume 65)

Summary

The wing-engine configuration is aerodynamically designed by the WINDES, inverse design code developed by Takanashi combined with the multi-block Navier-Stokes solver. The jet plume is considered in the analysis mode and the effect of the jet on/off is discussed. The inverse design method used here improves the L/D performance. Although the target MDD is not achieved, the MDD is also improved.

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References

  1. [1]
    Sawada, K., Takanashi, S, “A Numerical Investigation on Wing/Nacelle Interfarences of USB Configuration”, AIAA Paper 87–0455, 1987.Google Scholar
  2. [2]
    Takanashi, S., “A Theoretical Design Method for Three-Dimensional Transonic Wings”, NAL TR-830, 1984 in Japanese,Google Scholar
  3. [3]
    Kamiya, N., J. Japan Soc. Aeronautics and Spacesciences, Vol.27, No.311, 1979, pp.627–637 in Japanese.CrossRefGoogle Scholar
  4. [4]
    Kamiya, N., “On the Drag Divergence of Two-Dimensional Airfoils at Transonic Speeds”, NAL TR-299, 1973 in Japanese.Google Scholar
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    Eggleston, B, Poole, R.J., Jones, D.J., Khalid, M., “Thick Supercritical Airfoils with Low Drag and Natural Laminar Flow”, J. Aircraft, Vol.24, June 1987, pp.405–410.CrossRefGoogle Scholar

Copyright information

© Friedr. Vieweg & Sohn Verlagsgesellschaft mbH, Braunschweig/Wiesbaden 1999

Authors and Affiliations

  • Hitoshi Takahashi
    • 1
  • Susumu Takanashi
    • 1
  • Takuji Kishimoto
    • 2
  • Kenji Hayama
    • 2
  • Eiji Shima
    • 2
  1. 1.National Aerospace LaboratoryChofu City, TokyoJapan
  2. 2.Kawasaki Heavy Industries LTD.Kakamigahara City, Gifu-Pref.Japan

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