A RANS solver is presented to numerically simulate the viscous wake of an appended revolution body with guide vane propeller at the Reynolds number 10 7. The k ε turbulence model together with wall function is used. The resulting finite difference equations are solved by SIMPLEC and ADI. The technique of rising up the bottom surface is presented to overcome radial contraction problem in Cartesian coordinate system. The three dimensional body forces are separately adopted to model the affection of the guide vane and propeller. The detailed flow characteristics,especially the counter swirl component generated by the guide vane in the propeller inflow, are numerically seized successfully. Compared with the experimental data, The computational axial velocity on the propeller disk plane comes up to engineering requirement. A RANS solver is presented to numerically simulate the viscous wake of an appended revolution body with guide vane propeller at the Reynolds number 10 7. The k ε turbulence model together with wall function is used. The resulting finite difference equations are solved by SIMPLEC and the ADI. The technique of rising up the bottom surface is presented to overcome radial contraction problem in the Cartesian coordinate system. The three dimensional body forces are separately adopted to model the affection of the guide vane and propeller. The detailed flow characteristics, especially the counter Compared with the experimental data, The computational axial velocity on the propeller disk plane comes up to engineering requirement.