A composite wall consists of two plates A and B placed in series normal to the flow of heat. The thermal conductivities are \( k_A \) and \( k_B \) and the specific heat capacities are \( C_{pA} \) and \( C_{pB} \), for plates A and B respectively. Plate B has twice the thickness of plate A. At steady state, the temperature difference across plate A is greater than that across plate B when: