You are talking about 2 different shear failure modes for the different materials. The code approximation allowing a check at d from the support for reinforced concrete is simply there because, under most common design situations, the shear will not be critical between this point and the support face due to the fact that the angle of the compression strut is rising so they let you out of checking for shear in this region in these cases. That does not mean there is no shear there, just that it will not be critical in those cases.
This is explained very well (with diagrams) in ACI Clause R11.1.3.1.
In normal situations, a flexure shear crack will start in the top surface at the critical section for shear and extend diagonally to the support face at the bottom of the member. At points closer to the suport, the angle of the compression strut will rise and the shear capacity will increase faster than the uniform load shear will increase.
So, for uniform loading and correctly aligned supports, it is permissable to design for a critical section at d from the column face and assume that the design between the column face and the critical section requires the same reinforcement as at the critical section.
If heavy loads are applied between the support face and the critical section, then the shear must be checked at the support face (fig R11.1.3.1 (f)), also if there is no diagonal compression into the support. This shear check will be similar to a Deep Beam shear design and failure would be by direct shear rather than flexure shear as would occur at points outside the critical section.
In steel design, I presume you are checking for direct shear all of the time, rather than flexure shear as you ar in concrete design, as a direct shear failure can occur at any cross-section, so you need to check it at the support face and all points between.
British, Eurocode2 and Australian codes all allow for increased shear capacity in the region from 2d to the support face (this assumes a 30degree compression strut rather than the 45degree compression strut implied by the critical section being located at d from the support), but do require a check at the support face for non-uniform loads in the region of the support.