Modeling Of The Heat Transfer In Bypass Transitional Boundary Layer Flows

Modeling of the Heat Transfer in Bypass Transitional Boundary-layer Flows

Modeling of the Heat Transfer in Bypass Transitional Boundary-layer Flows

Modeling of the Heat Transfer in Bypass Transitional Boundary-Layer Flows

A low Reynolds number k-epsilon turbulence model and conditioned momentum, energy and turbulence equations were used to predict bypass transition heat transfer on a flat plate in a high-disturbance environment with zero pressure gradient. The use of conditioned equations was demonstrated to be an improvement over the use of the global-time-averaged equations for the calculation of velocity profiles and turbulence intensity profiles in the transition region of a boundary layer. The approach of conditioned equations is extended to include heat transfer and a modeling of transition events is used to predict transition onset and the extent of transition on a flat plate. The events, which describe the boundary layer at the leading edge, result in boundary-layer regions consisting of: (1) the laminar, (2) pseudolaminar, (3) transitional, and (4) turbulent boundary layers. The modeled transition events were incorporated into the TEXSTAN 2-D boundary-layer code which is used to numerically predict the heat transfer. The numerical predictions in general compared well with the experimental data and revealed areas where additional experimental information is needed. Simon, Frederick F. and Stephens, Craig A. Glenn Research Center NASA-TP-3170, E-6046, NAS 1.60:3170 RTOP 505-62-52...