Splitflow: A 3D unstructured cartesian/ prismatic grid CFD code for complex geometries

Sieve L. Karman

Research output: Contribution to conferencePaperpeer-review

99 Scopus citations

Abstract

A computational fluid dynamics (CFD) code, named SPLITFLOW, is described which makes use of a hybrid grid system to discretize complex 3D geometries. The primary grid system is an unstructured Cartesian grid, automatically generated by the code using recursive cell subdivision. This grid system is sufficient for computing Euler solutions about extremely complex 3D geometries. A secondary grid system, using triangular-prismatic elements, may be added for resolving the boundary layer region near surfaces of solid bodies for Navier-Stokes analyses. A description of the methods used to generate the grids and solve the governing equations is provided. Several example cases are provided, demonstrating the ability of the method to produce accurate solutions about complex geometries with very little pre-processing required by the user.

Original languageEnglish
StatePublished - 1995
Externally publishedYes
Event33rd Aerospace Sciences Meeting and Exhibit, 1995 - Reno, United States
Duration: Jan 9 1995Jan 12 1995

Conference

Conference33rd Aerospace Sciences Meeting and Exhibit, 1995
Country/TerritoryUnited States
CityReno
Period01/9/9501/12/95

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