A General Method for Calculating Three-dimensional Compressible Laminar and Turbulent Boundary Layers on Arbitrary Wings PDF Download
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Author: Tuncer Cebeci
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 98
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Book Description
Author: Tuncer Cebeci
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 98
Get Book Here
Book Description
Author: Tuncer Cebeci
Publisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 31
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Book Description
Author: Tuncer Cebeci
Publisher:
ISBN:
Category :
Languages : en
Pages : 37
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Book Description
The report presents a general method for computing three-dimensional laminar and boundary-layer flows in Cartesian coordinates. In the equations, the Reynolds shear stress terms are modeled by an eddy-viscosity formulation developed by the author. A very efficient two-point finite-difference method was used to solve the governing equations. The accuracy of the method is investigated for laminar and turbulent flows. (Author).
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 68
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Book Description
The report presents a general method for solving the laminar and turbulent boundary layer equations for swept infinite cylinders and for small cross flows. In the equations the Reynolds shear stress terms are eliminated by using an eddy viscosity concept. An efficient two-point finite-difference method used earlier by Keller and Cebeci for two dimensional flows is used to solve the governing equations. The method has been programmed on the IBM 370/165. (Author).
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 68
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Book Description
Author: Tuncer Cebeci
Publisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 31
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Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 182
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Book Description
Author: Tuncer Cebeci
Publisher:
ISBN:
Category :
Languages : en
Pages : 32
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Book Description
This report summarizes the third phase of studies conducted on the computation of three-dimensional incompressible laminar and turbulent boundary layers. Solutions of the governing equations in curvilinear orthogonal coordinates are presented for a curved rectangular duct. In addition the small-cross-flow method developed by Cebeci, Kaups, and Mosinskis is applied to compute the boundary layer on a cargo ship hull. The method uses the eddy-viscosity concept to model the Reynolds shear-stress terms and uses a very efficient two-point finite-differnce method to solve the governing equations.
Author: Tuncer Cebeci
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 63
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Book Description
The report presents a general method for solving the laminar and turbulent boundary layer equations for swept infinite cylinders and for small cross flows. In the equations the Reynolds shear stress terms are eliminated by using an eddy viscosity concept. An efficient two-point finite-difference method used earlier by Keller and Cebeci for two dimensional flows is used to solve the governing equations. The method has been programmed on the IBM 370/165. (Author).
Author: Tuncer Cebeci
Publisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 25
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Book Description
