1) pressure of afterburning chamber
补燃室压强
1.
Meanwhile,the tandency of change of specific impulse along with pressure of afterburning chamber were analyzed.
研究了固体火箭冲压发动机的理论性能,采用编制的热力计算程序对含铝镁和含硼贫氧推进剂进行了计算,分析了在设计点处补燃室温度、冻结流比冲、平衡流比冲随空燃比变化的趋势,以及比冲随补燃室压强变化的趋势。
2) afterburning chamber
补燃室
1.
Effects of fuel-gas jetting modes on mixing effectiveness in the afterburning chamber of solid rocket ramjets;
燃气喷射方式对冲压发动机补燃室掺混效果的影响
2.
Numerical simulation of mixing and combustion in afterburning chamber for ringed-propellant solid rocket ramjet engine was done by standard κ-ε two equation turbulent models.
文中采用标准κ-ε双方程湍流模型数值模拟一种环向进气的固体火箭冲压发动机补燃室的掺混燃烧过程,考虑了补燃室的出口反压、空燃比和燃气喷射角度等设计参数对燃烧流场的影响,结果表明:增大出口反压和空燃比,有利于补燃室内掺混和燃烧的进行;增大燃气喷射角度,补燃室头部温度升高,燃料停留时间增大,对燃烧流场特性影响不大。
3) Secondary combustion chamber
补燃室
1.
Flame temperature measurement in secondary combustion chamber based on image processing;
基于图像处理技术的补燃室火焰温度场测量
2.
Analysis of the powdered carbon combustibility in secondary combustion chamber for rocket ramjet engine;
碳粉燃料在火箭冲压发动机补燃室内燃烧特性的分析
3.
Research on the Secondary Combustion Chamber Operation Process of Boron-Based Propellant Ducted Rockets;
含硼推进剂固体火箭冲压发动机补燃室工作过程研究
4) afterburner
[英]['ɑ:ftəbɜ:nə(r)] [美]['æftɚ'bɝnɚ]
补燃室
1.
Analysis on aluminum-water combustion in afterburner of water ramjet
水冲压发动机补燃室铝水燃烧分析
2.
The numerical simulation of turbulent combustion in the afterburner of solid rocket ramjet was performed by applying the probability density function non -premixed mode.
应用概率密度函数非预混模型,对固体火箭冲压发动机补燃室内的湍流燃烧进行了数值模拟。
5) afterburning chamber length
补燃室长度
1.
Influence of afterburning chamber length on secondary combustion for solid ducted rocket motor;
补燃室长度对固冲发动机二次燃烧的影响
6) after-burning chamber configuration
补燃室结构
补充资料：焦炉炭化室墙的火焰焊补
焦炉炭化室墙的火焰焊补
5矿。焦炉炭化窒墙蜘火嬲埠补
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条