A Method for Computing Boundary-layer Flows, Including Normal Pressure Gradient and Longitudinal Curvature Effects

A Method for Computing Boundary-layer Flows, Including Normal Pressure Gradient and Longitudinal Curvature Effects PDF Author: Arloe W. Mayne (Jr.)
Publisher:
ISBN:
Category : Curvature
Languages : en
Pages : 40

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A Method for Computing Boundary-layer Flows, Including Normal Pressure Gradient and Longitudinal Curvature Effects

A Method for Computing Boundary-layer Flows, Including Normal Pressure Gradient and Longitudinal Curvature Effects PDF Author: Arloe W. Mayne (Jr.)
Publisher:
ISBN:
Category : Curvature
Languages : en
Pages : 40

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A Method for Computing Boundary-Layer Flows, Including Normal Pressure Gradient and Longitudinal Curvature Effects

A Method for Computing Boundary-Layer Flows, Including Normal Pressure Gradient and Longitudinal Curvature Effects PDF Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 0

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A method is presented for computing laminar and turbulent boundary-layer flows, including normal pressure gradient and longitudinal curvature as well as compressibility, transverse curvature, and other effects. The governing equations are transformed using the (omega squared) transformation to a von Mises form and solved using an implicit finite-difference scheme. The method is validated by comparing results with experimental data and results of other methods of computation.

Compressible Turbulent Boundary Layer Computations for Flow with Longitudinal Curvature

Compressible Turbulent Boundary Layer Computations for Flow with Longitudinal Curvature PDF Author: Walter B. Sturek
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 32

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A numerical study has been performed using a finite-difference boundary layer computer program that includes corrections to the equations of motion for longitudinal curvature and allows the static pressure to be specified as a known function of x and y. Calculations with and without the corrections for longitudinal curvature and pressure gradient normal to be the local surface have been compared to experimental measurements of a supersonic turbulent boundary layer flow over a surface with concave longitudinal curvature. Substantially improved agreement with experimental measurements is obtained for the calculations including corrections for wall curvature and pressure gradient normal to the local surface for density profile, skin friction coefficient, and boundary-layer integral properties.

COSMIC Software Catalog

COSMIC Software Catalog PDF Author:
Publisher:
ISBN:
Category : Computer software
Languages : en
Pages : 444

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Applied Mechanics Reviews

Applied Mechanics Reviews PDF Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 592

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U.S. Government Research Reports

U.S. Government Research Reports PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1064

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Technical Abstract Bulletin

Technical Abstract Bulletin PDF Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Military art and science
Languages : en
Pages : 1540

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Government Reports Announcements

Government Reports Announcements PDF Author:
Publisher:
ISBN:
Category : Technology
Languages : en
Pages : 232

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 960

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Calculation Methods for Compressible Turbulent Boundary Layers, 1976

Calculation Methods for Compressible Turbulent Boundary Layers, 1976 PDF Author: Dennis M. Bushnell
Publisher:
ISBN:
Category : Compressibility
Languages : en
Pages : 156

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