24th Congress of International Council of the Aeronautical Sciences, 29 August-3, September 2004, Yokohama, Japan
Paper ICAS 2004-3.6.1 (St.)

CURVATURE EFFECTS IN THE CURVED DUCT FOR THE COMPRESSIBLE VISCOUS FLOW

K. Ozaki, H. Maekawa*
Hiroshima University; *Hiroshima University, Japan

Keywords: compressible flow, curvature effects, transition

In this paper, non-reflecting boundary conditions based on characteristic boundary conditions for the three dimensional compressible Navier-Stokes equations (hereafter referred as NSCBC), especially outflow boundary conditions, are examined and numerical tests for a curved duct flow are made.

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