| 1. | The location of the instability zones is dictated by the combustor geometry and the steady-state combustion characteristics .
不稳定性区域的位置取决于燃烧室几何特性和稳定燃烧特性。 |
| 2. | The sensitive time lag theory circumvents the problems inherent in the description of unsteady combustion by use of a simplified two-parameter response function .
敏感时滞理论用简化的双参数响应函数来描述不稳定燃烧，从而绕过了某些固有的难点。 |
| 3. | Afterburner systems, designed to operate up to a stoichiometric overall mixture strength, are always fairly close to combustion instability or screech .
要使加力燃烧系统在理论化学组成量的总混合浓度下还在一直工作，这样的设计通常都很接近于不稳定燃烧或振荡燃烧。 |
| 4. | Fem numerical analysis for instability combustion in a firebox
燃烧腔不稳定燃烧的有限元数值分析 |
| 5. | Scs stabilized combustion system
稳定燃烧方式 |
| 6. | Key technonlogy of the steady combustion of anthracite in cement rotary furnaces
无烟煤在水泥回转窑中稳定燃烧的关键技术 |
| 7. | Numerical investigation of kerosene - droplet ' s instable combustion in oxidizer - rich gas
煤油液滴在富氧燃气中不稳定燃烧的数值研究 |
| 8. | The nozzle mix burners feature short flames , wide turndown ranges and very stable combustion
烧嘴混合炉头具有短焰，宽范围，非常稳定燃烧的特点。 |
| 9. | The experiment results indicate : when the velocity of propellant drops belows 40 m / s , the researched nozzles can obtain stably burning blaze
实验结果表明，喷雾液滴速度小于40m s时，所研究的同轴喷嘴可以获得稳定燃烧的火焰。 |
| 10. | Numerical simulations for different grain models show that the high frequency longitudinal acoustic oscillations could he generated at the moment of pressure filling
摘要固体火箭发动机中声波振荡是引起不稳定燃烧的一个重要原因。 |
