24th Congress of International Council of the Aeronautical Sciences, 29 August-3, September 2004, Yokohama, Japan
Paper ICAS 2004-2.6.R.1

NUMERICAL SIMULATION OF SUPERSONIC INTAKE USING STRUCTURED-UNSTRUCTURED ZONAL APPROACH

M. Kanazaki, H. Fujiwara, Y. Ito*, T. Fujita**, S. Obayashi***, K. Nakahashi**
Institute of Space Technology and Aeronautics, Japan Aerospace Exploration Agency, Japan; *Dept. of Mechanical Engineering, University of Alabama, USA; **Department of Aeronautics and Space Engineering, Tohoku University, Japan; ***Institute of Fluid Scie???????????!???

Keywords: Engine/Airframe Integration, Supersonic Intake, CFD, Zonal Approach

To perform a practical simulation, it is necessary to consider not only the nacelle-only configuration but also the engine/airframe configuration. In this paper, numerical simulation method for the prediction of supersonic intake performance using structured-unstructured zonal approach is discussed.

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