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- connular combustor 环管燃烧室
- Full-Scalc Liquid Fuel Ramjet Combustor Tests. 全尺寸液体冲压发动机燃烧室试验。
- Fig. 2 Schematic of the combustor model. 图2微燃烧器数值模型内部结构。
- Either stall or surge may result in combustor blowout. 不管是喘振或者爆音，都将引起燃烧室的熄火。
- This engine consists of an inlet, a combustor, and a nozzle. 这台发动机由一个进气道，一个燃烧室和一个尾喷管组成。
- This engine consists of an inlet , a combustor, and a nozzle. 这台发动机由一个进气道，一个燃烧室和一个尾喷管组成。
- The stability of the combustor was rated by use of bombs of varying sizes. 用不同装药量的爆炸弹对燃烧室的稳定性进行评定。
- Therefore by regulating swirl number of combustor NO emission caw be reduced. 因此;适当调整燃烧室的旋流数可以降低NO排放.
- The annular multi-hole radial jets have important effect on combustor liner. 环向径向射流对燃烧室火焰筒内的流场有着重要的影响。
- The crucial step for CST combustion is the selection of combustor... 该技术用于热交换器,亦是节能领域一新举。
- The backside of underprop is dangerous area of the front combustor casing. 结果表明,前机匣的支板后缘为危险区域;
- The combustor resonance properties are portrayed by instability zones, one z one for each acoustic mode. 燃烧室的共振特性用不稳定区表示每种声振型都有一个这样的区域。
- It was found that an increase in the stability of the combustor was obtained simply by gelling the hydrazine. 发现简单地通过肼胶化的方法可使燃烧室的稳定性提高。
- Compared with other natural gas combustor, this combustor can generate the second combustion and form circumfluence of smoke. 同一般天然气燃烧器相比,这种燃烧器既能产生二段燃烧,又能促进一定量的烟气回流。
- The combustor resonance properties are portrayed by instability zones, one zone for each acoustic mode. 燃烧室的共振特性用不稳定区表示,每种声振型都有一个这样的区域。
- 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。
- The fragmentation influences the char combustion behavior in a fluidized bed combustor. 摘要流化床燃烧中破碎特性影响了焦炭的燃烧。
- Elastoplastic finite element analysis and low cycle fatigue life prediction of an engine combustor case were completed. 对某发动机燃烧室外套进行了弹塑性有限元分析和低循环疲劳寿命预测。
- In this paper,the numerical simulation results are derived for the turbulent combustor. 本文给出了湍流燃烧室的数值模拟。
- In this system combustible premixed gases change their direction periodically, and flow into a combustor from two ends. 在该系统中,可燃预混气周期性换向,分别从两端流入燃烧器。
