The Compressible Laminar Boundary Layer with Fluid Injection

The Compressible Laminar Boundary Layer with Fluid Injection
Author: George M. Low
Publisher:
Total Pages: 38
Release: 1955
Genre: Aerodynamic heating
ISBN:

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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.

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.

AFOSR.

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

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