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

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Recent Development of Aerodynamic Design Methodologies

Part of the book series: Notes on Numerical Fluid Mechanics (NNFM) ((NONUFM,volume 65))

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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. Sawada, K., Takanashi, S, “A Numerical Investigation on Wing/Nacelle Interfarences of USB Configuration”, AIAA Paper 87–0455, 1987.

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  2. Takanashi, S., “A Theoretical Design Method for Three-Dimensional Transonic Wings”, NAL TR-830, 1984 in Japanese,

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  3. Kamiya, N., J. Japan Soc. Aeronautics and Spacesciences, Vol.27, No.311, 1979, pp.627–637 in Japanese.

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  4. Kamiya, N., “On the Drag Divergence of Two-Dimensional Airfoils at Transonic Speeds”, NAL TR-299, 1973 in Japanese.

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  5. 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.

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Author information

Authors and Affiliations

  1. National Aerospace Laboratory, 7-44-1, Jindaiji-Higashi-Machi, Chofu City, Tokyo, 182-8522, Japan

    Hitoshi Takahashi & Susumu Takanashi

  2. Kawasaki Heavy Industries LTD., 1, Kawasaki-Cho, Kakamigahara City, Gifu-Pref., 504-8710, Japan

    Takuji Kishimoto, Kenji Hayama & Eiji Shima

Authors
  1. Hitoshi Takahashi
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  2. Susumu Takanashi
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  3. Takuji Kishimoto
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  4. Kenji Hayama
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  5. Eiji Shima
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Editor information

Kozo Fujii George S. Dulikravich

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

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Takahashi, H., Takanashi, S., Kishimoto, T., Hayama, K., Shima, E. (1999). Aerodynamic Design of Wing-Engine Configuration under Effect of Jet Plume. In: Fujii, K., Dulikravich, G.S. (eds) Recent Development of Aerodynamic Design Methodologies. Notes on Numerical Fluid Mechanics (NNFM), vol 65. Vieweg+Teubner Verlag. https://doi.org/10.1007/978-3-322-89952-1_10

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  • DOI: https://doi.org/10.1007/978-3-322-89952-1_10

  • Publisher Name: Vieweg+Teubner Verlag

  • Print ISBN: 978-3-322-89954-5

  • Online ISBN: 978-3-322-89952-1

  • eBook Packages: Springer Book Archive

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