Journal ArticleDOI
Some aspects of high-speed blunt body flow computations with Roe scheme
S. K. Saxena,K. Ravi +1 more
Reads0
Chats0
TLDR
In this paper, an upwind total variation diminishing formulation of the Roe Riemann solver within the cell-centered finite volume approach was used for three-dimensional supersonic and hypersonic inviscid blunt body flow computations.Abstract:
This paper discusses some aspects of three-dimensional supersonic and hypersonic inviscid blunt body flow computations. The method used is based on the solution of the Euler equations employing an explicit, upwind total variation diminishing formulation of the Roe Riemann solver within the cell-centered finite volume approach. A comparative study of various total variation diminishing limiters and entropy fixes is carried out to identify the most appropriate combination. The effect of using cell spacing in the total variation diminishing extrapolations is highlighted. Furthermore, a Mach number dependence and grid sensitivity study is carried out on various total variation diminishing limiters scaled with mesh spacing. Local time stepping and code parallelization has been employed to accelerate convergence in terms of effective wall clock times.read more
Citations
More filters
Journal ArticleDOI
Computational Fluid Dynamics Algorithms for Unsteady Shock-Induced Combustion, Part 1: Validation
TL;DR: In this article, the authors developed a fully implicit and time-accurate computational dynamics code for the analysis of reactive e ow systems, where Euler equations and species conservation equations are used as the governing equations.
Journal ArticleDOI
A new approach of a limiting process for multi-dimensional flows
TL;DR: e-MLP has a number of advantages, as it incorporates useful features of MLP limiter such as multi-dimensional monotonicity and straightforward extensionality to higher order interpolation and is robust against shock instability.
Journal ArticleDOI
Computational Analysis of Inlet Aerodynamics for a Hypersonic Research Vehicle
TL;DR: In this article, the authors carried out Reynolds-averaged Navier-Stokes computations of flow through the inlet of a hypersonic research vehicle with a view to accomplish detailed aerodynamic analysis.
Proceedings ArticleDOI
An Improved Roe Scheme for Real Gas Flows
SK Saxena,Manoj T. Nair +1 more
TL;DR: In this paper, a Reynolds Averaged Navier-Stokes code has been developed for this purpose employing an improved Roe scheme which is very robust and does not require any entropy x. The present work emphasises numerical simulation of hypersonic o w with chemical non-equilibrium.
Proceedings ArticleDOI
Implementation and testing of Spalart-Allmaras model in a multi-block code
S. Saxena,M. Nair +1 more
References
More filters
Journal ArticleDOI
High Resolution Schemes Using Flux Limiters for Hyperbolic Conservation Laws
TL;DR: The technique of obtaining high resolution, second order, oscillation free (TVD), explicit scalar difference schemes, by the addition of a limited antidiffusive flux to a first order scheme is described in this article.
Journal ArticleDOI
Towards the ultimate conservative difference scheme. II. Monotonicity and conservation combined in a second-order scheme
TL;DR: Fromm's second-order scheme for integrating the linear convection equation is made monotonic through the inclusion of nonlinear feedback terms in this paper, where care is taken to keep the scheme in conservation form.
A comparative study of computational methods in cosmic gas dynamics
TL;DR: In this article, the authors apply several commonly used algorithms and one new algorithm, to a representative problem in galactic gas dynamics, and a careful choice of the algorithm used in a calculation is found to be of the utmost importance in obtaining reliable results.
Book ChapterDOI
A comparative study of computational methods in cosmic gas dynamics
TL;DR: In this article, the authors apply several commonly used algorithms and one new algorithm, to a representative problem in galactic gas dynamics, and a careful choice of the algorithm used in a calculation is found to be of the utmost importance in obtaining reliable results.
Journal ArticleDOI
Self adjusting grid methods for one-dimensional hyperbolic conservation laws☆
Ami Harten,James M. Hyman +1 more
TL;DR: It is shown how to automatically adjust the grid to follow the dynamics of the numerical solution of hyperbolic conservation laws using Godunov's and Roe's methods on a self-adjusting mesh.
Related Papers (5)
Short Note: On the dissipation mechanism of upwind-schemes in the low Mach number regime: A comparison between Roe and HLL
The influence of cell geometry on the accuracy of upwind schemes in the low mach number regime
Felix Rieper,Georg Bader +1 more