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.

 

 

Contour of Mach Number Around of Cone-Cylinder (M=1.2).

 

Comparison of Mach Number On Symmetry Plane Between 3D-Euler-Code and FLUENT.

 

Contour of Cp on Onera-M6 Wing and Symmetry Plane (M=0.7).

 

Comparison of Cp On Section( y/L=0.2) of  Wing  Between 3D-Euler-Code and FLUENT.