Author: Ralph Alois Seban
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 182
Book Description
Heat Transfer to Turbulent Boundary Layers in High Velocity Flow
Author: Ralph Alois Seban
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 182
Book Description
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 182
Book Description
Survey of Boundary Layer Heat Transfer at High Velocities and High Temperatures
Author: Ernst Rudolf Georg Eckert
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 118
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 118
Book Description
Heat Transfer by Convection in High Velocity Laminar and Turbulent Boundary Layer Flow
Author: Ai Duc Duong
Publisher:
ISBN:
Category :
Languages : en
Pages : 134
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 134
Book Description
A Review of High-speed, Convective, Heat-transfer Computation Methods
Author: Michael E. Tauber
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 44
Book Description
Heat Transfer to Turbulent Boundary Layers with a Variable Free-stream Velocity
Author: Lloyd H. Back
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 272
Book Description
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 272
Book Description
Turbulent Flows and Heat Transfer
Author: Chia-Ch'iao Lin
Publisher: Princeton University Press
ISBN: 1400879418
Category : Science
Languages : en
Pages : 570
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.
Publisher: Princeton University Press
ISBN: 1400879418
Category : Science
Languages : en
Pages : 570
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.
Similar Solutions for Turbulent Boundary Layer with Large Favorble Pressures Gradients (nozzle Flow with Heat Transfer)
Author: James F. Schmidt
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 68
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).
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 68
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).
Analysis of Turbulent Flow and Heat Transfer on a Flat Plate at High Mach Numbers with Variable Fluid Properties
Author: R. G. Deissler
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 42
Book Description
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 42
Book Description
An Investigation of the High Speed Turbulent Boundary Layer with Heat Transfer and Arbitrary Pressure Gradient: The Compressibility transformation
Author: Constantino Economos
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 52
Book Description
This report investigates the behavior of high speed turbulent boundary layer with heat transfer and streamwise pressure gradient.
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 52
Book Description
This report investigates the behavior of high speed turbulent boundary layer with heat transfer and streamwise pressure gradient.
An Investigation of the High Speed Turbulent Boundary Layer with Heat Transfer and Arbitrary Pressure Gradient. Part 2 - The Compressibility Transformation - General Considerations
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 52
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 52
Book Description