Heat Transfer in a Laminar Compressible Boundary Layer on a Porous Flat Plate with Variable Fluid Injection PDF Download
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Author: Nathan Ness
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 34
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Book Description
Author: Nathan Ness
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 34
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Book Description
Author: S. W. Yuan
Publisher:
ISBN:
Category :
Languages : en
Pages : 24
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Book Description
Author: George M. Low
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 38
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Book Description
A solution of the equations of the compressible laminar boundary layer including the effects of transpiration cooling is presented. The analysis applies to the flow over an isothermal porous plate with a velocity of fluid injection proportional to the reciprocal of the square root of the distance from the leading edge.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 31
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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: Shao Wen Yuan
Publisher:
ISBN:
Category :
Languages : en
Pages : 16
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Author: H. Shuh
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 28
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Book Description
In connection with Pohlhausen's solution for the temperature field on the flat plate, a series of formulas were indicated by means of which the velocity and temperature field for variable physical characteristics can be computed by an integral equation and an iteration method based on it. With it, the following cases were solved: On the assumption that the viscosity simply varies with the temperature while the other fluid properties remain constant, the velocity and temperature field on the heated and cooled plate, respectively, was computed at the Prandtl numbers 12.5 and 100 (viscous fluids). A closer study of these two cases resulted in general relations: The calculations for a gas of Pr number 0.7 (air) were conducted on the assumption that all fluid properties vary with the temperature, and the velocities are low enough for the heat of friction to be discounted. The result was a thickening of the boundary layers, but no appreciable modification in shearing stress or heat-transfer coefficient.
Author:
Publisher:
ISBN:
Category : Jet propulsion
Languages : en
Pages : 580
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Book Description
Author: United States. Air Force. Office of Scientific Research
Publisher:
ISBN:
Category : Research
Languages : en
Pages : 1190
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Author: H. S. Mickley
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 166
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Book Description
The effect on the boundary layer of sucking or blowing air through a porous flat plate into or out of a main air stream flowing parallel to the plate was studied theoretically and experimentally.
