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Proceedings ArticleDOI

Recent enhancements to OVERFLOW

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TLDR
The purpose of this paper is to highlight some recent enhancements that have been made to the Navier-Stokes code OVERFLOW, in three major areas: a multigrid method, for convergence acceleration; a lowMach preconditioning algorithm, for converge acceleration and solution quality improvement for low Mach number flows; and a matrix dissipation algorithm for solution quality improved.
Abstract
The purpose of this paper is to highlight some recent enhancements that have been made to the Navier-Stokes code OVERFLOW. The enhancements we are concerned with are in three major areas: a multigrid method, for convergence acceleration; a lowMach preconditioning algorithm, for convergence acceleration and solution quality improvement for low Mach number flows; and a matrix dissipation algorithm for solution quality improvement. We will describe these methods and show examples of their efficacy.

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Citations
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Proceedings ArticleDOI

Development of an iterative PNS code for separated flows

TL;DR: A new iterative parabolized Navier-Stokes (PNS) algorithm is being developed to efficiently compute supersonic viscous flowfields with embedded separated regions that is successfully incorporated into NASA’s upwind PNS (UPS) code.
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An efficient solver for the RANS equations and a one-equation turbulence model

TL;DR: It is demonstrated that the two-dimensional RANS equations and a transport-type equation for turbulence modeling can be efficiently solved with an indirectly coupled algorithm that uses RK/Implicit schemes.
Proceedings ArticleDOI

Navier-Stokes analyses of a 747 high lift configuration

TL;DR: Three-dimensional Navier-Stokes solutions obtained using the OVERFLOW code for a 747PD high lift configuration are presented and the chimera grid methodology used in generating the 747PD grid system is described.

Efé cient Newton -Krylov Solver for Aerodynamic Computations

TL;DR: In this paper, an inexact Newton-Krylov algorithm is presented for the computation of steady two-dimensional aerodynamic flow, which uses the preconditioned, restarted generalized minimal residual method in matrix-free form to solve the linear system arising at each Newton iteration.
Proceedings ArticleDOI

Design, manufacturing and test of a plug nozzle rocket engine

TL;DR: In this article, the authors present the design, manufacture and test of a small 1000 lbf ablative annular plug nozzle rocket engine, which was developed by students with the help from faculty and industry professionals as part of the California Launch Vehicle Education Initiative.
References
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Book

Matrix computations

Gene H. Golub
Book

An Introduction to Multigrid Methods

P. Wesseling
TL;DR: These notes were written for an introductory course on the application of multigrid methods to elliptic and hyperbolic partial differential equations for engineers, physicists and applied mathematicians, restricting ourselves to finite volume and finite difference discretization.
Journal ArticleDOI

A diagonal form of an implicit approximate-factorization algorithm

TL;DR: The modification transforms the coupled system of equations into an uncoupled diagonal form that requires less computational work and has an important effect on the application of implicit finite-difference schemes to vector processors.
Journal ArticleDOI

Preconditioned methods for solving the incompressible low speed compressible equations

TL;DR: It is sown that the resultant incompressible equations form a symmetric hyperbolic system and so are well posed, and several generalizations to the compressible equations are presented which extend previous results.
Proceedings ArticleDOI

A 3-D Chimera Grid Embedding Technique

TL;DR: A three-dimensional (3-D) chimera grid-embedding technique that simplifies the construction of computational grids about complex geometries by solution of the Euler equations for the transonic flow about a wing/body, wing/ body/tail, and a configuration of three ellipsoidal bodies is described.
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