Similarity Solutions for Small Cross Flows in Laminar Compressible Boundary Layers PDF Download
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Author: Ivan E. Beckwith
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 34
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Book Description
Author: Ivan E. Beckwith
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 34
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Book Description
Author: Ivan E. Beckwith
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 26
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Book Description
![Similarity Solutions for Small Cross Flows in Laminar Compressible Boundary Layers [with List of References] PDF](https://books.google.com/books/content/images/frontcover/yoKCyAEACAAJ?fife=w80-h100)
Author:
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 26
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Book Description
Author:
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 1
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Book Description
Author: Nathaniel B. Cohen
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 72
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Book Description
Correlations of the transport property estimates of NASA TR R-50 are employed to determine locally similar solutions of the laminar boundary-layer equations for air in chemical equilibrium. Exact solutions for flat-plate flow, axisymmetric stagnation flow, and stagnation flow for yawed infinite cylinder are obtained, and a correlation formula for the heat-transfer distribution function for arbitrary favorable pressure gradient is determined. Extension to three-dimensional flows with small cross flow is briefly described.
Author: Arthur G. Hansen
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 716
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Book Description
Solutions of mainstream flow patterns for all possible incompressible laminar-boundary-layer flows having classical similarity with respect to rectangular coordinate systems are derived. These solutions, which apply to a wide range of flows, are summarized in table form.
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 72
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Book Description
Author: James W. Christian
Publisher:
ISBN:
Category :
Languages : en
Pages : 103
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Book Description
Governing equations are formulated for laminar compressible similar boundary layers with heat transfer, adverse pressure gradient, and constant cross flow. These equations are expressed in finite difference form and solved numerically. Solutions are found for attached and separated flows in adverse pressure gradients for nine combinations of cross flow and heat transfer. The purpose of these solutions is to provide understanding of how cross flow alters the two-dimensional similar results. Solutions are presented in the form of temperature profiles, main flow and cross flow velocity profiles, and global quantities; wall velocity and temperature gradients, displacement thickness, momentum thicknesses, and form factor.
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1304
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Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 912
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