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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Author: E. R. G. Eckert
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 330
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Book Description
Author: E. R. G. Eckert
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 330
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Book Description
Author: R. J. Brun
Publisher:
ISBN:
Category :
Languages : en
Pages : 43
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 43
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages :
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Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Author:
Publisher:
ISBN:
Category : Cold regions
Languages : en
Pages : 360
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Book Description
Author: United States. Federal Aviation Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 64
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Book Description
Author: John B. Howe
Publisher:
ISBN:
Category : Clouds
Languages : en
Pages : 28
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 580
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 508
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Book Description
Author: Robert G. Deissler
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 608
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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.
