| タイトル | Application of integration algorithms in a parallel processing environment for the simulation of jet engines |
| 本文（外部サイト） | http://hdl.handle.net/2060/19820006976 |
| 著者（英） | Milner, E. J.; Krosel, S. M. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1982-01-01 |
| 言語 | eng |
| 内容記述 | The application of Predictor corrector integration algorithms developed for the digital parallel processing environment are investigated. The algorithms are implemented and evaluated through the use of a software simulator which provides an approximate representation of the parallel processing hardware. Test cases which focus on the use of the algorithms are presented and a specific application using a linear model of a turbofan engine is considered. Results are presented showing the effects of integration step size and the number of processors on simulation accuracy. Real time performance, interprocessor communication, and algorithm startup are also discussed. |
| NASA分類 | NUMERICAL ANALYSIS |
| レポートNO | 82N14849
E-1059
NASA-TM-82746 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/167314 |
