Abstract
The least-squares (LS) method is often used in computational aerodynamics to reconstruct a given function at certain points of a computational grid. In this paper we discuss the accuracy of the LS approximation on highly stretched meshes that. are inherent in computational aerodynamics. A new definition of a distant point in a LS reconstruction stencil will be given in order to explain the poor performance of the method in a boundary layer region. Namely, based on the concept of outliers widely used in the statistics, we demonstrate that; the definition of a distant point in a LS reconstruction stencil should take into account the solution properties and it cannot rely upon the geometric shape of the stencil only. Our approach is illustrated with numerical examples.
| Original language | English |
|---|---|
| Pages (from-to) | 449-462 |
| Number of pages | 14 |
| Journal | International Journal of Computational Methods |
| Volume | 05 |
| Issue number | 03 |
| DOIs | |
| Publication status | Published - 1 Jan 2008 |
Keywords
- solution reconstruction
- outliers
- stretched mesh
- Least-squares method
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