A FORTRAN Program of the Truckenbrodt Laminar and Turbulent Boundary Layer Calculation PDF Download
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Author: Joe F. Thompson
Publisher:
ISBN:
Category : FORTRAN (Computer program language)
Languages : en
Pages : 66
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Book Description
Author: Joe F. Thompson
Publisher:
ISBN:
Category : FORTRAN (Computer program language)
Languages : en
Pages : 66
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Book Description
Author: William D. McNally
Publisher:
ISBN:
Category : Laminar flow
Languages : en
Pages : 124
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Book Description
Author: Patricia Anton
Publisher:
ISBN:
Category :
Languages : en
Pages : 56
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Book Description
A FORTRAN computer program for the numerical solution of the compressible laminar boundary layer equations is presented. The method of solution employed is an implicite finite difference integration scheme, by which the velocity components and the temperature are determined in the physical plane. All possible boundary conditions and arbitrary initial conditions can be treated. The pertinent aspects of the solution are discussed in detail. Operating instructions are presented along with a flow chart and the listing of the program and sample calculations are included for check-out purposes. (Author).
Author: Arthur J. Glassman
Publisher:
ISBN:
Category : Aircraft gas-turbines
Languages : en
Pages : 164
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Book Description
Author: Richard Eppler
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 50
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Book Description
Author: H. J. Herring
Publisher:
ISBN:
Category : Laminar flow
Languages : en
Pages : 100
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 160
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Book Description
Author: H. J. Herring
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 0
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Book Description
Author: C. Hah
Publisher:
ISBN:
Category :
Languages : en
Pages : 180
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Book Description
Author: J. Schneider
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 106
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Book Description
A computer program is described capable of determining the properties of a compressible turbulent boundary layer with pressure gradient and heat transfer. The program treats the two-dimensional problem assuming perfect gas and Crocco integral energy solution. A compressibility transformation is applied to the equation for the conservation of mass and momentum, which relates this flow to a low speed constant property flow with simultaneous mass transfer and pressure gradient. The resulting system of describing equations consists of eight ordinary differential equations which are solved numerically. For Part 1, see N72-12226; for Part 2, see N72-15264.
