Calculation Methods for Compressible Turbulent Boundary Layers, 1976 PDF Download
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Author: Dennis M. Bushnell
Publisher:
ISBN:
Category : Compressibility
Languages : en
Pages : 156
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Book Description
Author: Dennis M. Bushnell
Publisher:
ISBN:
Category : Compressibility
Languages : en
Pages : 156
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Book Description
Author: Dennis M. Bushnell
Publisher:
ISBN:
Category : Turbulent boundary layer
Languages : en
Pages : 156
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Book Description
Author: H. James Herring
Publisher:
ISBN:
Category :
Languages : en
Pages : 99
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Book Description
Author: Shimer Zane Pinckney
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 68
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Book Description
Author: H. James Herring
Publisher:
ISBN:
Category : Turbulent boundary layer
Languages : en
Pages : 124
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Book Description
Author: M. C. Altstatt
Publisher:
ISBN:
Category : Compressibility
Languages : en
Pages : 46
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Book Description
A computer code for a turbulent, compressible boundary-layer method, capable of carrying out computations in a region of separated flow, is developed and tested. The procedure after separation is to specify either friction velocity or boundary-layer thickness as an independent variable and obtain external velocity as a dependent variable. This requires a trial and error alternation of the specified variable in order to match the desired experimental or computed external velocity. Satisfactorily results were obtained by this method in the analysis of certain specialized cases of separated flow. (Author).
Author: Neal Tetervin
Publisher:
ISBN:
Category : Enthalpy
Languages : en
Pages : 96
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Book Description
The method predicts that a positive pressure gradient increases and a negative pressure gradient decreases the ratio of Stanton number to friction coefficient. The Crocco relation between the velocity and total enthalpy for a non-adiabatic surface and zero pressure gradient is generalized to non-zero pressure gradient. The relation between the velocity and the total enthalpy varies markedly from the flat plate Crocco relation as the pressure gradient departs from zero. The magnitude of the variation depends on the velocity profile shape parameter. (Author).
Author:
Publisher:
ISBN:
Category : Compressibility
Languages : en
Pages : 580
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Book Description
Author: Larry L. Lynes
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 146
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1282
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Book Description
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.
