The 3D Euler code was developed by using Roe's average first order upwind method. Obtained results were compared FLUENT (Explicit First order upwind). Flow field Simulation around cone-cylinder body and Onera-M6 wing and comparison Cp were shown.
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Contour of Mach Number Around of Cone-Cylinder (M=1.2).
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Comparison of Mach Number On Symmetry Plane Between 3D-Euler-Code and FLUENT.
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Contour of Cp on Onera-M6 Wing and Symmetry Plane (M=0.7).
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Comparison of Cp On Section( y/L=0.2) of Wing Between 3D-Euler-Code and FLUENT.
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