| タイトル | Computer Modeling Of Atomization |
| 著者（英） | Ibrahim, E.; Yang, H.; Przekwas, A.; Krishnan, A.; Giridharan, M.; Lee, J.; Cheuch, S. |
| 著者所属（英） | NASA Marshall Space Flight Center |
| 発行日 | 1994-07-01 |
| 言語 | eng |
| 内容記述 | Improved mathematical models based on fundamental principles of conservation of mass, energy, and momentum developed for use in computer simulation of atomization of jets of liquid fuel in rocket engines. Models also used to study atomization in terrestrial applications; prove especially useful in designing improved industrial sprays - humidifier water sprays, chemical process sprays, and sprays of molten metal. Because present improved mathematical models based on first principles, they are minimally dependent on empirical correlations and better able to represent hot-flow conditions that prevail in rocket engines and are too severe to be accessible for detailed experimentation. |
| NASA分類 | MECHANICS |
| レポートNO | 94B10358
MFS-28721 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/313242 |
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