In SST k omega model the flow is resolved up to the wall. For this the y+ =1. However, in some cases where the solution is converged and showing fairly good results, the y+ values are different.
Off course you should check the values. The dimensionless wall distance y+ should be approximately = 1 if you adopt a near wall model approach (mesh refinement) and it can lies between 50 and 500 if you adopt a wall function approach.
Some factors should be considered which the most significant is the turbulent boundary layer. If you're using any kind of low Reynolds turbulence model considering enhanced wall treatment (as your K-W SST model), so you need to make sure that you stay in the laminar sub layer region where velocity profiles is assumed to be laminar and viscous stress dominates the wall shear which means (Y+
y+ is the near wall grid spacing nondimensionalised using the so called shear stress velocity. It is effectively a Reynolds number. In order to resolve the laminar sub layer you need a value of less than 1. However, you do not have to slavishly apply the rule. Normally I find that an average value over the surface of y+ =1 is adequate. But the best approach is to find out for yourself: run the code twice with two different y+ values and see what happens to the flow field. If it does not change, in any way you care about, then the coarse grid is adequate!
Off course you should check the values. The dimensionless wall distance y+ should be approximately = 1 if you adopt a near wall model approach (mesh refinement) and it can lies between 50 and 500 if you adopt a wall function approach.
Parag ji, You should always check your y+ value as your near wall results will greatly depends on y+. It should be 1 for most of the cases, but it may be acceptable as long as your fist grid point lie in the range of viscous sub laye i.e. y+