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 Download

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Report

Report
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 50
Release: 1957
Genre: Aeronautics
ISBN:

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Annual Report - National Advisory Committee for Aeronautics

Annual Report - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages:
Release: 1957
Genre: Aeronautics
ISBN:

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


Aircraft Ice Protection

Aircraft Ice Protection
Author: United States. Federal Aviation Administration
Publisher:
Total Pages: 64
Release: 1971
Genre: Aeronautics
ISBN:

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CRREL Report

CRREL Report
Author:
Publisher:
Total Pages: 360
Release: 1991
Genre: Cold regions
ISBN:

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Index of NACA Technical Publications

Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 580
Release: 1956
Genre: Aeronautics
ISBN:

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Special Report

Special Report
Author:
Publisher:
Total Pages: 396
Release: 1983
Genre: Arctic regions
ISBN:

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Research Abstracts and Reclassification Notice

Research Abstracts and Reclassification Notice
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 508
Release: 1954
Genre: Aeronautics
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.