ENERGY PROFILES AND HEAT - TRANSFER IN THE SIMILAR LAMINAR BOUNDARY LAYER WITH PRESSURE GRADIENT AND VARIABLE WALL TEMPERATURE.
POLITECNICO DI TORINO (ITALY) ISTITUTO DI MECCANICA APPLICATA AERODINAMICA E GASDINAMICA
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The total energy equation for the two-dimensional steady laminar boundary layer is solved by means of two functions one sufficient for low-speed flows, and one for high-speed flows. Outer-velocity and wall-enthalpy gradients are considered, in the field of the similar flows. Numerical results are tabulated and plotted. Author
- Fluid Mechanics