| タイトル | Error Reduction Program |
| 本文（外部サイト） | http://hdl.handle.net/2060/19850019273 |
| 著者（英） | Gosman, A. D.; Chiappetta, L. M.; Syed, S. A. |
| 著者所属（英） | Pratt and Whitney Aircraft |
| 発行日 | 1985-01-11 |
| 言語 | eng |
| 内容記述 | The details of a study to select, incorporate and evaluate the best available finite difference scheme to reduce numerical error in combustor performance evaluation codes are described. The combustor performance computer programs chosen were the two dimensional and three dimensional versions of Pratt & Whitney's TEACH code. The criteria used to select schemes required that the difference equations mirror the properties of the governing differential equation, be more accurate than the current hybrid difference scheme, be stable and economical, be compatible with TEACH codes, use only modest amounts of additional storage, and be relatively simple. The methods of assessment used in the selection process consisted of examination of the difference equation, evaluation of the properties of the coefficient matrix, Taylor series analysis, and performance on model problems. Five schemes from the literature and three schemes developed during the course of the study were evaluated. This effort resulted in the incorporation of a scheme in 3D-TEACH which is usuallly more accurate than the hybrid differencing method and never less accurate. |
| NASA分類 | NUMERICAL ANALYSIS |
| レポートNO | 85N27584
NAS 1.26:174776
NASA-CR-174776
PWA-5928-25 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/156309 |
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