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Journal ArticleDOI

A space-marching method for the computation of viscous internal flows

T. R. Govindan, +1 more
- 02 Jan 1988 - 
- Vol. 16, Iss: 1, pp 21-39
TLDR
In this article, the Navier-Stokes equations have been formulated as an initial value problem by neglecting the effects of streamwise diffusion and treating the streamwise pressure gradient as a known source term.
About
This article is published in Computers & Fluids.The article was published on 1988-01-02. It has received 7 citations till now. The article focuses on the topics: Pressure-correction method & Computational fluid dynamics.

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Citations
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Journal ArticleDOI

General Three-Dimensional Viscous Primary/Secondary Flow Analysis

TL;DR: In this paper, generalized primary/secondary flow equations are derived as an approximation to the Navier-Stokes equations for three-dimensional viscous flows with a dominant flow direction, and a sequentially decoupled implicit algorithm has been developed that exploits the form of the primary and secondary flow equations to obtain decouple subsets of equations through choices for dependent variables, the sequence of equations, and the linearization scheme.
Journal ArticleDOI

Numerical Analysis of Heated Channel Flows by a Space-Marching Finite Volume Technique

TL;DR: In this paper, a parabolized Navier-Stokes equation is used for cooling properties of real fluids in channels, based on a finite volume approach, which uses a modified Roe's approximate Riemann solver for a fluid governed by a generic equation of state.
Journal ArticleDOI

Three-dimensional turbulent near-wall flows in streamwise corners: Current state and questions

TL;DR: In this article, the structure, properties and main regularities of 3D near-wall turbulent flows in a wide range of variable conditions and basic parameters are discussed. And the main factors on the structure of the flow in streamwise corners are analyzed, including the effectiveness of flow control by streamwise vortices in the junction regions of aerodynamic surfaces.
Proceedings ArticleDOI

On Further Development of an Unstructured Space-Marching Technique

TL;DR: The present work is aimed at further refining of the Nakahashi and Saitoh’s space marching method, and the results of the application of the improved method to supersonic flows in air-breathing engine inlets and ram accelerators are presented.

Development of secondary flow in a curved rectangular duct

TL;DR: In this article, an improved finite difference scheme for solving parabolized Navier-Stokes equations is presented, which has its origin in the work of Briley, which is based on ADI method to march the solution in the streamwise direction.
References
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Book

Viscous Fluid Flow

TL;DR: In this article, the stability of Laminar Boundary Layer Flow Appendices has been investigated in Cylindrical and Spherical Coordinates of Incompressible Newtonian Fluids.
Journal ArticleDOI

A calculation procedure for heat, mass and momentum transfer in three-dimensional parabolic flows

TL;DR: In this article, a general, numerical, marching procedure is presented for the calculation of the transport processes in three-dimensional flows characterised by the presence of one coordinate in which physical influences are exerted in only one direction.
Book

Navier-Stokes Equations: Theory and Numerical Analysis

TL;DR: This paper presents thediscretization of the Navier-Stokes Equations: General Stability and Convergence Theorems, and describes the development of the Curl Operator and its application to the Steady-State Naviers' Equations.
Journal ArticleDOI

The prediction of laminarization with a two-equation model of turbulence

TL;DR: In this article, the local turbulent viscosity is determined from the solution of transport equations for the turbulence kinetic energy and the energy dissipation rate, and the predicted hydrodynamic and heat-transfer development of the boundary layers is in close agreement with the measured behaviour.
Proceedings ArticleDOI

Thin-layer approximation and algebraic model for separated turbulent flows

B. Baldwin, +1 more
TL;DR: In this article, an algebraic turbulence model for two-and three-dimensional separated flows is specified that avoids the necessity for finding the edge of the boundary layer, and compared with experiment for an incident shock on a flat plate, separated flow over a compression corner, and transonic flow over an airfoil.
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