位置：成果数据库 > 会议 > 会议详情页
Experimental study of arc root behavior in direct current plasma torches
  • 所属机构名称：中国科学院力学研究所
  • 会议名称：2nd International Workshop on Non-equilibrium Flows
  • 成果类型：会议
  • 相关项目：影响电弧加热发动机寿命和效率的关键热物理问题研究
作者： Huang heji|Pan Wenxia|Wu Chengkang|
同会议论文项目
影响电弧加热发动机寿命和效率的关键热物理问题研究
期刊论文 50 会议论文 65 获奖 2 专利 9
同项目会议论文
喷管长度对氨电弧加热发动机性能影响的模拟研究
Volt-ampere characteristics, nozzle temperature and thruster performances in a low power argon arcje
Plasma and Electrode Emissions from a 1 kW Hydrogen-Nitrogen Arcjet Thruster
等离子体活性烧结纳米碳化硅涂层的实验研究
Modeling of the heat transfer and flow characteristics of a low-power hydrogen arc-heated thruster
电弧加热推进系统试验研究进展
氢氮电弧加热发动机内部温度测量
稀薄气体效应对高速飞行器气动性能的影响
低功率电弧加热发动机喷管扩张段内壁面温度测量
等离子体国防高技术应用
低中功率氢电弧加热发动机内传热与流动特性比较研究
小型等离子体风洞材料烧蚀行为研究
Nonequilibrium modeling of the low-power argon arcjet
Roe格式有限差分方法求解MHD方程组的初步研究
小功率氨电弧推力器性能研究
Contact discontinuity and shock wave: a nonequilibrium solution
氮等离子体双温度输运性质计算
Low-power arcjet thruster with N2/H2/NH3 propellants
低功率电弧加热推力器阳极弧根行为研究
电弧加热发动机内的流动、传热与传质研究进展
Kinetic studies of gas flows
低功率电弧加热推力器喷管温度与性能
A fixed arc length direct current plasma torch for reduced pressure deposition of thin films
Plume Parameters and Thruster Properties of a Low Power Arcjet
氢电弧加热发动机能量转化过程比较研究
Numerical Simulation of a Low-power Hydrazine Arcjet Thruster
Experimental study on energy dissipation in a 1 kW arcjet thruster
推力器射流动压分布检测与分析
电弧加热发动机羽流电子温度与电子数密度的双静电探针测量,
星际航行推进系统概览
氩电弧加热发动机喷管温度与伏安特性
千瓦级氩电弧加热发动机的二维数值模拟
减压层流等离子体射流温度的热电偶测量
Two-dimensional LTE modeling of a low-power argon arcjet thruster
Simulation of gas flow over a micro cylinder
Measured temperature of a laminar plasma jet by using thermocouple at reduced pressure
千瓦级电弧加热推力器羽流动压测量
Configuration optimization of hypersonic vehicles under transitional flow conditions
Monitoring of fluctuations in a direct current argon plasma jet at reduced pressure by double-electr
Development of a cell size relaxed scheme for the direct simulation monte carlo method
Development of arc root attachment in the nozzle of 1 kW N2 and H2-N2 arcjet thrusters
减压等离子体特性研究
Effects of propellant type on low power arcjet thruster performance
Development of a cell size relaxed scheme for the direct simulation monte carlo method
Development of a cell size relaxed scheme for the direct simulation monte carlo method
Development of a cell size relaxed scheme for the direct simulation monte carlo method
氪等离子体双温度输运性质计算
Unsteady phenomena in a non-transferred dc arc plasma generator
低功率氮氢电弧加热发动机内气体反混合效应的初步模拟研究
Very low-power arcjet thruster operated with ammonia propellant
Modeling studies to compare the flow and heat transfer characteristics of the low-power simulated am
Unsteady phenomena in a non-transferred dc arc plasma generated at reduced pressure
Two-temperature thermodynamic and transport properties of hydrogen plasmas
低功率氮氢电弧加热发动机内反混合效应的数值模拟研究
Numerical simulation of low and medium power arcjet thrusters
氩电弧加热发动机羽流温度测量
磁场对高超声速钝头扰流影响的数值模拟
低功率氦电弧加热发动机的数值模拟研究
氮氢混合物双温度等离子体热力学性质
On the validity of the Boltzmann-BGK model
氧原子对反向流动扩散火焰传热与流动特性影响的模拟研究
Effects of viscosity, compressibility and rarefaction in several gas flows
Numerical modeling of heat transfer and plasma flow in a low power arcjet thruster
电弧加热发动机约束通道内热壅塞现象研究