What you have above is not correct... understeer gradient is well, a gradient - a rate of change. It is expressed in degrees per G. Whereas what you have written in the final expression on the far right is the difference between two angles.
Barring that however, you would indeed replace "Cf" by "Clf + Crf" simple as that.
@ Jersey tom ..The expression the extreme right shoud be (alpha_front-alpha_rear)/lateral accleration , I forgot to write the latter term while posting the previous post. Thanks for the correction.
@Greg locock .. thanks for elaborating the expression and clarifing my doubt.
Well coming back to yaw rate. This is something that has been confusing me for very long time and somehow even after reading many articles I am unable to convince myself. In steady-state yaw rate is given by Velocity times the path curvature. This is what is confusing me. Considering a case in which the vehicle goes in a straight line (infinite radius turn). Now if a constant wind blows in a direction perpendicular to the vehicle heading direction, then the front and rear tires will react to the lateral force due to the wind and some slip angle will be induced. The front and rear slip angle may or may not be same , depending on the front and rear axle weight distribution and the tire stiffness. Consider a situation in which the front axle developes more slip angle as compares to the rear, so in this case the vehicle will start to move in the curve away from the wind (understeer), so this will induce a side-slip angle (due to the tire slip angles) and a yaw rate (depending on the relative front and rear slip angles , since the vehicle moves in a curved path) at the center of mass. So this case shows that yaw rate is dependant on the slip angles, then why is it not true for steady state cornering ? In that case the force due to wind will be replaced by the cornering force (mv^2 / R) . PLease correct me if I am going wrong somewhere.
Regards!