Abstract:We describe a Cartesian grid strategy for the study of three dimensional inviscid flows about arbitrary geometries that uses both conventional and CAD/CAM surface geometry databases. Initial applications of the technique are presented. The elimination of the body-fitted constraint allows the grid generation process to be automated, significantly reducing the time and effort required to develop suitable computational grids for inviscid flowfield simulations.
“…The Cartesian, cell-based approach has been demonstrated extensively for a wide variety of inviscid flows [11,8,9,16,15,19,22,23] and has been assessed for accu- …”
Section: Iiib Validation Of the Euler Solvermentioning
confidence: 99%
“…The Cartesian, cell-based approach has been used for solving a variety of problems, and variants of the approach have proven to be quite useful for computing both unsteady [6,7,26,27,5,10,25]and steady [11,8,9,16,15,19,22] …”
“…The Cartesian, cell-based approach has been demonstrated extensively for a wide variety of inviscid flows [11,8,9,16,15,19,22,23] and has been assessed for accu- …”
Section: Iiib Validation Of the Euler Solvermentioning
confidence: 99%
“…The Cartesian, cell-based approach has been used for solving a variety of problems, and variants of the approach have proven to be quite useful for computing both unsteady [6,7,26,27,5,10,25]and steady [11,8,9,16,15,19,22] …”
“…[8,31,60,7]), or unstructured meshes (see e.g. [65,33,44,42,43]). Large parallel codes have also been written and used in commercial applications, e.g.…”
“…The existing Cartesian grids CFD software often work with Euler and potential equations and not suitable for viscous flow [1,2]. Viscous Cartesian grid and NS equation are essential for viscous flow simulations.…”
In this paper, a 3D anisotropic Cartesian grid generation method is produced. With this technique, the fine parts of missiles that have small geometry scale can be described with high quality, which of course will improve the aerodynamics prediction accuracy. Viscous Cartesian grids generating of several stand missile models and simulations with finite volume method demonstrate the success of current method. It is found that the prediction accuracy of aerodynamics coefficients are greatly improved companied with results obtained with traditional Cartesian grid generation method, especially for roller moment and yawing moment.
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