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 PDF Author: L. M. Albacete
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ISBN:
Category : Heat
Languages : en
Pages : 68

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Book Description
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.

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 PDF Author: L. M. Albacete
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 68

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Book Description
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.

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Category : Government publications
Languages : en
Pages : 1062

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Technical Abstract Bulletin

Technical Abstract Bulletin PDF Author: Defense Documentation Center (U.S.)
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Category : Science
Languages : en
Pages : 784

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Critical Evaluation of Transition from Laminar to Turbulent Shear Layers with Emphasis on Hypersonically Traveling Bodies

Critical Evaluation of Transition from Laminar to Turbulent Shear Layers with Emphasis on Hypersonically Traveling Bodies PDF Author: Mark Vladimir Morkovin (|d)
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Category : Aerodynamics, Hypersonic
Languages : en
Pages : 152

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Scientific and Technical Aerospace Reports PDF Author:
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Category : Aeronautics
Languages : en
Pages : 1040

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Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

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Category : Heat
Languages : en
Pages : 80

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Turbulent Boundary Layer Displacement Effects in Hypersonic Flow PDF Author: Richard Martin Grabow
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Category : Aerodynamics, Hypersonic
Languages : en
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Category : Cavitation
Languages : en
Pages : 60

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U.S. Government Research & Development Reports PDF Author:
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ISBN:
Category : Science
Languages : en
Pages : 784

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U. S. Government Research and Development Reports

U. S. Government Research and Development Reports PDF Author:
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ISBN:
Category : Science
Languages : en
Pages : 1150

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