Ahmed Body for 35 degree slant angle
 

I have done an aerodynamic simulation for an Ahmed Body with a slant angle of 35 degrees and inlet velocity of 60 m/s in Ansys Fluent.
I computed the Cd and Cl values and got 0.35365859 and 0.13842661 respectively.
Will anyone help me to compare these values and confirm my solution. If there is any issue in the values please let me know.