24th Congress of International Council of the Aeronautical Sciences, 29 August-3, September 2004, Yokohama, Japan
Paper ICAS 2004-2.3.4

NUMERICAL SIMULATION OF HIGH LIFT CONFIGURATION USING UNSTRUCTURED MESH METHOD

M. Murayama, K. Yamamoto
Institute of Space Technology and Aeronautics, Japan Aerospace Exploration Agency, Japan

Keywords: high-lift configurations, CFD, unstructured mesh

In this paper, computations around 2D/3D high-lift configurations are performed on structured and unstructured meshes for improvement of the accuracy of the flow analyses. By comparison with the results, some ways to improve the reliability on structured and unstructured meshes are discussed.

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