Analysis of Turbulent Flow and Heat Transfer on a Flat Plate at High Mach Numbers with Variable Fluid Properties
Author | : R. G. Deissler |
Publisher | : |
Total Pages | : 42 |
Release | : 1959 |
Genre | : Aerodynamic heating |
ISBN | : |
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Author | : R. G. Deissler |
Publisher | : |
Total Pages | : 42 |
Release | : 1959 |
Genre | : Aerodynamic heating |
ISBN | : |
Author | : Robert G. Deissler |
Publisher | : |
Total Pages | : 608 |
Release | : 1958 |
Genre | : Aerodynamic heating |
ISBN | : |
A previous analysis of turbulent heat transfer and flow with variable fluid properties in smooth passages is extended to flow over a flat plate at high Mach numbers. Velocity and temperature distributions are calculated for a boundary layer in which the effects of both frictional heating and external heat transfer are appreciable. The viscosity and thermal conductivity are assumed to vary as a power of the temperature, while the Prandtl number and specific heat are taken as constant. Skin-friction and heat-transfer coefficients are calculated and compared with the incompressible values. The relation between boundary-layer thickness and distance along the plate is obtained for various Mach numbers. The analytical results are compared with representative experimental data.
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 300 |
Release | : 1960 |
Genre | : |
ISBN | : |
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 498 |
Release | : 1958 |
Genre | : |
ISBN | : |
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 550 |
Release | : 1958 |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 388 |
Release | : 1959 |
Genre | : Aeronautics |
ISBN | : |