Heat Transfer to Turbulent Boundary Layers in High Velocity Flow PDF Download
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Author: Ralph Alois Seban
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 182
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Author: Ralph Alois Seban
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 182
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Book Description
Author: Ernst Rudolf Georg Eckert
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 118
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Author: Ai Duc Duong
Publisher:
ISBN:
Category :
Languages : en
Pages : 134
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Author: Michael E. Tauber
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 44
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Book Description
Author: Lloyd H. Back
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 272
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Book Description
Author: Chia-Ch'iao Lin
Publisher: Princeton University Press
ISBN: 1400879418
Category : Science
Languages : en
Pages : 570
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Book Description
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.
Author: James F. Schmidt
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 68
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Book Description
In order to provide a relatively simple heat-transfer prediction along a nozzle, a differential (similar-solution) analysis for the turbulent boundary layer is developed. This analysis along with a new correlation for the turbulent Prandtl number gives good agreement of the predicted with the measured heat transfer in the throat and supersonic regiono f the nozzle. Also, the boundary-layer variables (heat transfer, etc. ) can be calculated at any arbitrary location in the throat or supersonic region of the nozzle in less than a half minute of computing time (Lewis DCS 7094-7044).
Author: R. G. Deissler
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 42
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Author: Constantino Economos
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 52
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Book Description
This report investigates the behavior of high speed turbulent boundary layer with heat transfer and streamwise pressure gradient.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 52
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