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NASA NTRS · 20080032590

An Idealized, Single Radial Swirler, Lean-Direct-Injection (LDI) Concept Meshing Script

Abstract

To easily study combustor design parameters using computational fluid dynamics codes (CFD), a Gridgen Glyph-based macro (based on the Tcl scripting language) dubbed BladeMaker has been developed for the meshing of an idealized, single radial swirler, lean-direct-injection (LDI) combustor. BladeMaker is capable of taking in a number of parameters, such as blade width, blade tilt with respect to the perpendicular, swirler cup radius, and grid densities, and producing a three-dimensional meshed radial swirler with a can-annular (canned) combustor. This complex script produces a data format suitable for but not specific to the National Combustion Code (NCC), a state-of-the-art CFD code developed for reacting flow processes.

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BibTeXRIS

Iannetti, Anthony C., Thompson, Daniel. 2008-07-01. An Idealized, Single Radial Swirler, Lean-Direct-Injection (LDI) Concept Meshing Script. https://ntrs.nasa.gov/citations/20080032590

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