Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery 2000
DOI: 10.1115/2000-gt-0517
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Reducing Bottlenecks in the CAD-to-Mesh-to-Solution Cycle Time to Allow CFD to Participate in Design

Abstract: As CFD has matured to the point that it is capable of reliable and accurate flow simulation, attention is now firmly fixed on how best to deploy that CFD as part of a process to improve actual products. This “process” consists of capturing and controlling the geometry of a suitable portion of an aeroengine (eg a blade row, or an internal cooling system or a fan-plus-nacelle), building a mesh system, solving the flow and responding to an appropriately visualized flow field by changing or accepting the geometry.… Show more

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Cited by 14 publications
(11 citation statements)
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“…The code reads meshes generated from a suite of meshgeneration programs developed in-house. 41 It has been observed that sphere-sphere contact points may cause solution inaccuracy due to the generation of thin, unsuitable cells, or failure to generate cells at all. 32,42,43 This issue has been avoided by either under-sizing 44 or over-sizing 45 the spheres.…”
Section: Geometry and Meshingmentioning
confidence: 99%
“…The code reads meshes generated from a suite of meshgeneration programs developed in-house. 41 It has been observed that sphere-sphere contact points may cause solution inaccuracy due to the generation of thin, unsuitable cells, or failure to generate cells at all. 32,42,43 This issue has been avoided by either under-sizing 44 or over-sizing 45 the spheres.…”
Section: Geometry and Meshingmentioning
confidence: 99%
“…Our RANS solver ("NEWT") was written in the 1990's and applied extensively to turbomachinery, as described for example in Dawes [1992Dawes [ , 1993, Longley et al [2000], Angel et al [1998] and Jackson [1996]. Later, extensions were made to other application areas; see, for example, Kellar et al [1999], Dawes et al [2001], Smith at al [2003]. The solver was very simple and consisted of the Reynolds Averaged Navier Stokes equations discretised using a second order finite volume approach on an all-tetrahedral mesh with both a simple mixing length and also a low Reynolds number k- turbulence model.…”
Section: The Basic Unstructured Mesh Rans Flow Solvermentioning
confidence: 99%
“…Morishige and Takeuchi (1997) planed suitable tool track to manufacture impellers. Dawes et al (2001) did not only use three-dimensional CAD modeling but also constructed hexahedral grids for CFD computing. Nerurker et al (1996) proposed an impeller design method in which the parametric optimization technique was coupled with CFD analyses.…”
Section: Introductionmentioning
confidence: 99%