1) None equilibrium chemically reacting fluid fields
复燃流场
2) combustion flow field
燃烧流场
1.
In order to study the influence of the flame- holder layout on the outlet temperature distribution,combustion efficiency and total pressure loss,the numerical simulation of combustion flow field for a ramjet combustor was completed.
为了研究不同火焰稳定器布局对燃烧室流场特征和燃烧性能的影响,对某型亚燃冲压发动机燃烧室的三维湍流燃烧流场进行了数值模拟。
2.
The performance of the combustion flow field at the three conditions was analyzed for the gas turbine annular combustor.
根据改型后燃气轮机的结构特点建立了真实的三维计算几何模型;计算中采用SIMPLE算法,可利用k-ε双方程湍流模型、六通量辐射模型、非绝热概率密度函数(PDF)燃烧模型及热力型NO模型对燃烧流动进行数值模拟,分析了燃气轮机环形燃烧室在3种状态下燃烧流场的性能。
3.
The numerical simulation of combustion flow field for the plasma generator was performed by using eddy break up(EBU) combustion model,k-ε two-equation turbulent model and SIMPLEC algorithm.
采用漩涡破碎(EBU)燃烧模型、k-ε双方程湍流模型及SIMPLEC算法,对等离子发生器内部的燃烧流场进行了数值模拟,得到了关于等离子燃烧流场相关特性参数分布。
3) exhausted flow field
燃气流场
1.
A set of experimental studies were conducted to study complicated internal exhausted flow field generated by missile which was launched from a closed container-launcher.
为研究火箭导弹在封闭式储运发射箱内发射时 ,由于密封盖的反射作用使弹箱间隙内存在的复杂燃气流场 ,通过对测量数据进行子波分析 ,得到了管 (箱 )壁压力时间历程曲线中的燃气射流段是由射流激波振荡 (低频 )和射流噪声 (高频 )两种流动成分组合而成 ,激波振荡沿管壁向弹头方向是衰减的 ,它在低频段聚积的能量与起始冲击波一起都对储运发射箱式定向器具有破坏作用。
4) gas flow field
燃气流场
1.
Compared with other solid rocket engine, the nozzle of the solid rocket pulse has sharp curvature, which results in a complicated gas flow field, and without a heat-shield, which causes overheating in the structure of nozzle and nozzle pedestal.
与一般的固体火箭发动机相比,其喷管具有强曲率的特征,燃气流场异常复杂,无采用隔热防护层,造成喷管和喷管座结构的严重受热,机械性能大幅下降。
5) complex wake
复合流场
1.
The superposition between the helicopter rotor induced flow and the warship airwake leads to the formation of the complex wake,which affects the helicopter s control response and flight safety during take-off and landing from a warship.
直升机旋翼诱导流与舰船空气尾流叠加后形成复合流场,对直升机舰上起降时的操纵响应及飞行安全有很大的影响。
6) complex flow field
复杂流场
1.
The paper gives the measurements results of complex flow field about a delta wing coupled pitching and rolling oscillation at high amplitude in low speed wind tunnel .
给出 8 0°三角翼模型在低速风洞中实施俯仰 滚摆耦合大幅度振动的复杂流场测量结果 ,包括静态和动态、单自由度俯仰和滚摆、俯仰 滚摆耦合运动条件下的流动显示结果和强迫俯仰、自由滚摆条件下的滚转角时间历程测量结果。
2.
To better the application of PTV technique in complex surface flow field,an automatic image segmentation method based on frame difference and adaptive threshold was established,and particle signature identification was introduced,which bettered the effect of particle recognition and tracking in complex flow field.
为了改善粒子跟踪测速技术(PTV)在复杂流场测速中的应用效果,本文采用基于帧间差分和自适应阈值的自动图像分割技术,引入粒子的特征标识,改善了复杂流场中粒子识别与运动跟踪的效果;另外,通过流速滤波、插值处理,提高了流速测量的精度。
补充资料:死灰复燃
烧剩的灰烬重新燃烧起来。比喻消失或沉寂后重又兴起:死灰复燃,物有待尔|把事情做得干净点,免得死灰复燃,又生出麻烦来。
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