Impingement of Cloud Droplets on a Cylinder and Procedure for Measuring Liquid-water Content and Droplet Sizes in Supercooled Clouds by Rotating Multicylinder Method

Impingement of Cloud Droplets on a Cylinder and Procedure for Measuring Liquid-water Content and Droplet Sizes in Supercooled Clouds by Rotating Multicylinder Method PDF Author: E. R. G. Eckert
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ISBN:
Category : Aerodynamics
Languages : en
Pages : 330

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Index of NACA Technical Publications

Index of NACA Technical Publications PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 580

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Annual Report - National Advisory Committee for Aeronautics

Annual Report - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
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ISBN:
Category : Aeronautics
Languages : en
Pages :

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Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.

Research Abstracts and Reclassification Notice

Research Abstracts and Reclassification Notice PDF Author: United States. National Advisory Committee for Aeronautics
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ISBN:
Category : Aeronautics
Languages : en
Pages : 508

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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 PDF Author: Robert G. Deissler
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ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 608

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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.

Special Report

Special Report PDF Author:
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ISBN:
Category : Arctic regions
Languages : en
Pages : 396

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Technical Note - National Advisory Committee for Aeronautics

Technical Note - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
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ISBN:
Category : Aeronautics
Languages : en
Pages : 550

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Analysis of Three Liquid-metal Quality Measurement Techniques

Analysis of Three Liquid-metal Quality Measurement Techniques PDF Author: Ted W. Nyland
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ISBN:
Category : Calorimetry
Languages : en
Pages : 44

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Technical Note

Technical Note PDF Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 430

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On Possible Similarity Solutions for Three-dimensional Incompressible Laminar Boundary Layers

On Possible Similarity Solutions for Three-dimensional Incompressible Laminar Boundary Layers PDF Author: Arthur G. Hansen
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ISBN:
Category : Air flow
Languages : en
Pages : 716

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Book Description
Solutions of mainstream flow patterns for all possible incompressible laminar-boundary-layer flows having classical similarity with respect to rectangular coordinate systems are derived. These solutions, which apply to a wide range of flows, are summarized in table form.