A review of turbulent-boundary-layer heat transfer research at Stanford, 1958-1983
Abstract
For the past 25 years, there has existed in the Thermosciences Laboratory of the Mechanical Engineering Department of Stanford University a research program, primarily experimental, concerned with heat transfer through turbulent boundary layers. In the early phases of the program, the topics considered were the simple zero-pressure-gradient turbulent boundary layer with constant and with varying surface temperature, and the accelerated boundary layer. Later equilibrium boundary layers were considered along with factors affecting the boundary layer, taking into account transpired flows, flows with axial pressure gradients, transpiration, acceleration, deceleration, roughness, full-coverage film cooling, surface curvature, free convection, and mixed convection. A description is provided of the apparatus and techniques used, giving attention to the smooth plate rig, the rough plate rig, the full-coverage film cooling rig, the curvature rig, the concave wall rig, the mixed convection tunnel, and aspects of data reduction and uncertainty analysis.
- Publication:
-
IN: Advances in heat transfer. Volume 16 (A85-20501 07-34). Orlando
- Pub Date:
- 1984
- Bibcode:
- 1984aht....16..241M
- Keywords:
-
- Convective Heat Transfer;
- Film Cooling;
- Heat Transfer;
- Hydraulic Jets;
- Turbulent Boundary Layer;
- Acceleration;
- Couette Flow;
- Curvature;
- Data Reduction;
- Flow Velocity;
- Momentum Transfer;
- Nusselt Number;
- Prandtl Number;
- Reynolds Number;
- Stanton Number;
- Technology Assessment;
- Temperature Profiles;
- Transpiration;
- Fluid Mechanics and Heat Transfer