Analysis of Heat Transfer and Fluid Friction for Fully Developed Turbulent Flow of Supercritical Water with Variable Fluid Properties in a Smooth Tube

Analysis of Heat Transfer and Fluid Friction for Fully Developed Turbulent Flow of Supercritical Water with Variable Fluid Properties in a Smooth Tube
Author: Robert G. Deissler
Publisher:
Total Pages: 29
Release: 1953
Genre: Charts, diagrams, etc
ISBN:

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A previous analysis of turbulent flow and heat transfer for air with variable properties flowing in smooth tubes is generalized in order to make it applicable to supercritical water. The generalization is necessary because all the pertinent properties of supercritical water vary markedly with temperature. Calculated velocity and temperature distributions, as well as relations among Nusselt number, Reynolds number, and friction factor, are presented. The effect of variation of fluid properties across the tube on the Nusselt number and friction factor correlations can be eliminated by evaluating the properties at a reference temperature which is a function of both the wall temperature and the ratio of wall-to-bulk temperatures.

Analysis of Turbulent Heat Transfer, Mass Transfer, and Friction in Smooth Tubes at High Prandtl and Schmidt Numbers

Analysis of Turbulent Heat Transfer, Mass Transfer, and Friction in Smooth Tubes at High Prandtl and Schmidt Numbers
Author: Robert G. Deissler
Publisher:
Total Pages: 62
Release: 1954
Genre: Aerodynamic heating
ISBN:

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The expression for eddy diffusivity from a previous analysis was modified in order to account for the effect of kinematic viscosity in reducing the turbulence in the region close to a wall. By using the modified expression, good agreement was obtained between predicted and experimental results for heat and mass transfer at Prandtl and Schmidt numbers between 0.5 and 3000. The effects of length-to-diameter ratio and of variable viscosity were investigated for a wide range of Prandtl numbers.

NACA Research Memorandum

NACA Research Memorandum
Author:
Publisher:
Total Pages: 38
Release: 1953
Genre: Aerodynamics
ISBN:

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Analysis of Turbulent Flow and Heat Transfer on a Flat Plate at High Mach Numbers with Variable Fluid Properties

Analysis of Turbulent Flow and Heat Transfer on a Flat Plate at High Mach Numbers with Variable Fluid Properties
Author: Robert G. Deissler
Publisher:
Total Pages: 608
Release: 1958
Genre: Aerodynamic heating
ISBN:

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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.

Analysis of Turbulent Heat Transfer and Flow in the Entrance Regions of Smooth Passages

Analysis of Turbulent Heat Transfer and Flow in the Entrance Regions of Smooth Passages
Author: Robert G. Diessler
Publisher:
Total Pages: 90
Release: 1953
Genre: Air flow
ISBN:

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A previous analysis for fully developed turbulent heat transfer and flow with variable fluid properties is extended and applied to the entrance regions of smooth tubes and parallel flat plates. Integral heat-transfer and momentum equations are used for calculating the thicknesses of the thermal and flow boundary layers. The effect of variable properties is determined for the case of uniform heat flux, uniform initial temperature distribution, and fully developed velocity distribution. A number of ther cases in which the fluid properties are considered constant are analyzed. The predicted Nusselt numbers for air with a uniform wall temperature and uniform initial temperature and velocity distributions agree closely with experimentally determined values.

NASA Technical Note

NASA Technical Note
Author:
Publisher:
Total Pages: 416
Release: 1970
Genre:
ISBN:

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Technical Note

Technical Note
Author:
Publisher:
Total Pages: 378
Release: 1954
Genre: Aeronautics
ISBN:

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