Author: Robert G. DeisslerPublisher:
ISBN:
Category :
Languages : en
Pages : 24
Book Description
Analysis of Turbulent Flow and Heat Transfer in Noncircular Passages
Author: Robert G. DeisslerAnalysis of Turbulent Flow and Heat Transfer in Noncircular Passages
Author: Robert G. DeisslerPublisher:
ISBN:
Category : Heat
Languages : en
Pages : 0
Book Description
Analysis of Turbulent Flow and Heat Transfer in Noncircular Passages [with List of References]
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Author: Analysis of Turbulent Flow and Heat Transfer in Noncircular Passages
Author: Robert G. DeisslerAnalysis of Turbulent Flow and Heat Transfer on a Flat Plate at High Mach Numbers with Variable Fluid Properties
Author: Robert G. DeisslerPublisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 608
Book Description
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.
NASA Technical Report
Author: Analysis of Turbulent Heat Transfer and Flow in the Entrance Regions of Smooth Passages
Author: Robert G. DiesslerPublisher:
ISBN:
Category : Air flow
Languages : en
Pages : 90
Book Description
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
Author: Scientific and Technical Aerospace Reports
Author: Monthly Catalog of United States Government Publications
Author: Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1698
Book Description