On Available Calculation Procedures for Steady Three-dimensional Boundary Layers PDF Download
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Author: S. V. Patankar
Publisher:
ISBN:
Category :
Languages : en
Pages : 18
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Book Description
Author: S. V. Patankar
Publisher:
ISBN:
Category :
Languages : en
Pages : 18
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Book Description
Author: Richard Allen Burbank
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 280
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Book Description
Author: G. S. Raetz
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 33
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Book Description
A numerical method of calculating the laminar boundary layer on any three-dimensional surface in steady compressible flow is presented. This method can be applied readily on an automatic digital computer with any desired accuracy. It is valid at and near the usual singular points and lines of a surface as well as elsewhere. A principle clarifying various aspects of three-dimensional flow also is given. (Author).
Author: Theo Geis
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 96
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Author: Raymond Sedney
Publisher:
ISBN:
Category :
Languages : en
Pages : 54
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The study of three-dimensional boundary layers is synonymous with the study of cross flow or streamwise vorticity in the boundary layer. The research is concerned with the initial value problem for the 3-D boundary layer equations. Results are reported on exact solutions for the decay of streamwise vorticity, on a combined oil-flow--optical method of visualizing the surface flow field in the presence of 3D protuberances, and nonuniform behavior of the small crossflow approximation.
Author:
Publisher:
ISBN: 9789283504078
Category : Aerodynamics
Languages : en
Pages : 218
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Author: Omar Erkin Peremeci
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ISBN:
Category :
Languages : en
Pages :
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Author: Erik Janke
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ISBN:
Category :
Languages : en
Pages : 28
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Author: Bilal Hafeez Mughal
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ISBN:
Category :
Languages : en
Pages : 148
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Author: Charles R. Strom
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 136
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Book Description
The method of characteristics is formulated for the computation of the supersonic flow of an inviscid, reacting gas over a smooth three-dimensional body. Various methods of constructing networks of bicharacteristic lines are examined from the point of view of numerical stability and accuracy. A new method of forming the network, which consists of projecting forward along streamlines from data points on specified data planes, is found to be most easily adopted to the particular requirements of nonequilibrium chemistry. The general method was coded for the IBM 7090 computer and the program demonstrated for the case of an ideal gas. Calculations were made for the case of an ideal gas. Calculations were made for the flow about a spherical-tip 15 degree half-angle cone at 10 degree angle of attack and a generalized elliptical body at zero incidence. Since the program yields the pressure distribution along specified streamlines, it is straightforward, in principle, to link it to a finite-rate chemistry stream tube program to treat three-dimensional, nonequilibrium flows. (Author).
