| タイトル | Combustion stability with baffles, absorbers and velocity sensitive combustion |
| 本文（外部サイト） | http://hdl.handle.net/2060/19800009863 |
| 著者（英） | Mitchell, C. E. |
| 著者所属（英） | Colorado State Univ. |
| 発行日 | 1980-02-01 |
| 言語 | eng |
| 内容記述 | Analytical and computational techniques were developed to predict the stability behavior of liquid propellant rocket combustors using damping devices such as acoustic liners, slot absorbers, and injector face baffles. Models were developed to determine the frequency and decay rate of combustor oscillations, the spatial and temporal pressure waveforms, and the stability limits in terms of combustion response model parameters. |
| NASA分類 | INORGANIC AND PHYSICAL CHEMISTRY |
| レポートNO | 80N18128
NASA-CR-162803 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/173290 |
|
