Finite difference methods for reducing numerical diffusion in TEACH-type calculations
Abstract
A methodological evaluation for two-finite differencing schemes for computer-aided gas turbine design is presented. The two computational schemes include; a Bounded Skewed Finite Differencing Scheme (BSUDS); and a Quadratic Upwind Differencing Scheme (QSDS). In the evaluation, the derivations of the schemes were incorporated into two-dimensional and three-dimensional versions of the Teaching Axisymmetric Characteristics Heuristically (TEACH) computer code. Assessments were made according to performance criteria for the solution of problems of turbulent, laminar, and coannular turbulent flow. The specific performance criteria used in the evaluation were simplicity, accuracy, and computational economy. It is found that the BSUDS scheme performed better with respect to the criteria than the QUDS. Some of the reasons for the more successful performance BSUDS are discussed.
- Publication:
-
AIAA, Aerospace Sciences Meeting
- Pub Date:
- January 1985
- Bibcode:
- 1985aiaa.meetU....S
- Keywords:
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- Computational Fluid Dynamics;
- Computational Grids;
- Error Analysis;
- Finite Difference Theory;
- Applications Programs (Computers);
- Backward Facing Steps;
- Laminar Flow;
- Swirling;
- Turbulent Flow;
- Fluid Mechanics and Heat Transfer