Turbulent Flows and Heat Transfer

Turbulent Flows and Heat Transfer
Author: Chia-Ch'iao Lin
Publisher: Princeton University Press
Total Pages: 570
Release: 2015-12-08
Genre: Science
ISBN: 1400879418

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Volume V of the High Speed Aerodynamics and Jet Propulsion series. Topics include transition from laminar to turbulent flow; turbulent flow; statistical theories of turbulence; conduction of heat; convective heat transfer and friction in flow of liquids; convective heat transfer in gases; cooling by protective fluid films; physical basis of thermal radiation; and engineering calculations of radiant heat exchange. Originally published in 1959. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.

AFOSR.

AFOSR.
Author: United States. Air Force. Office of Scientific Research
Publisher:
Total Pages: 1190
Release: 1950
Genre: Research
ISBN:

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Technical Memorandum PIB

Technical Memorandum PIB
Author:
Publisher:
Total Pages: 580
Release: 1948
Genre: Jet propulsion
ISBN:

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Skin Friction and Heat Transfer Characteristics of the Compressible Laminar Boundary Layer with Injection of a Light, Medium, and Heavy Gas

Skin Friction and Heat Transfer Characteristics of the Compressible Laminar Boundary Layer with Injection of a Light, Medium, and Heavy Gas
Author: L. M. Albacete
Publisher:
Total Pages: 68
Release: 1967
Genre: Heat
ISBN:

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The effects of the injection of a light, medium, and heavy gas on the skin friction and heat transfer characteristics of the laminar boundary layer flow over a flat plate were investigated. This was done by a numerical solution of the governing differential equations for injection rate parameters of -0, -0. 1, -0.2; Mach numers from 0 to 3; and wall-to-stream temperature ratios of 0.25, 0.50, and 1.00. The results show that the selection of discrete injection systems must represent a favorable compromise between conflicting factors (such as small molecular weight and large molecular diameters) which influence the amount of reduction in skin friction and heat transfer desired.

Report

Report
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 36
Release: 1952
Genre: Aeronautics
ISBN:

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