Although the periodic or penetration descriptions of the turbulent boundary layer oversimplify this phenomenon by treating a complex statistical process in terms of some mean period, such models often lead to simple, accurate analytical relationships for evaluation of the important transport processes. A principal defect of these descriptions is the poor agreement observed between experiment and prediction for the case of heat or mass transfer with high Prandtl or Schmidt numbers. Katesbas and Gordon (1974) showed that improved agreement could be obtained by postulating Prandtl number dependency of the minimum sublayer decay thickness S1+ used by Meek and Baer (1970). The concept of a prandtl number dependent minimum penetration thickness is not very mechanistically satisfying, since it is postulated that the growth and decay of the boundary layer are dynamic processes. It is unlikely that such processes would be affected by the fluid Prandtl number or the Schmidt number for the mass transfer process. This deficiency of these formulations, as will be shown later, is the same defect of the early steady state models; the turbulent eddy diffusion in the viscous region of the sublayer was not considered.Because of the difficulty in formulation of the boundary condition for heat transfer at the position of the minimum decay thickness, earlier calculations for the heat transfer case of Meek and Baer (1973) were made by means of a numerical model which required solution of the temperature field over several growth and decay cycles. An adequate formulation of this difficult boundary condition can be obtained by recognition that in the region near the wall from 0 < y + < S1 +, the temperature field is the same at the beginning and the end of each cycle. If a quadratic temperature distribution is assumed in this region, an analytical representation of the developing temperature field can be obtained, and the constants in the assumed profile can be obtained since the temperature gradient at the wall and at Sl+ are the same at the beginning and end of each cycle. The wall temperature is assumed constant throughout the cycle, which is an adequate approximation for a metallic wall. Although quite complex, a closed form solution for a Stanton number can be obtained which is presented as Equation ( The assumption of a linear temperature profile yields a relationship which gives essentially equivalent results for 1 < Np,. < 200 and can be obtained from Equation ( l ) , since in this case Go = U. Equation (1) is easily evaluated by use of a computer and has some value for checking the numerical solutions. The Stanton number obtained by use of Equation (1) is in terms of the temperature difference between the wall and the fluid at tho position of the maximum growth distance of the laminar sublayer. By use of the logarithmic form of the ternperdure distribution in the turbulence core, as obtained fron mixing length theory, it is possible to use these Stantori numberis to obtain the result conventionally based on the mean strea...