期刊文献+

超声速电弧喷射器内等离子体流场的数值模拟 被引量:3

NUMERICAL SIMULATION ON THE INTERNAL PLASMA FLOW OF A SUPERSONIC ARCJET
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摘要 对一个以氮气为工作气体、在局域热力学平衡下的超声速电弧喷射器内等离子体流场进行了数值模拟。流动模型是耦合了电磁场的扩展N-S方程组。电场由电势方程近似反映,只考虑周向自感应磁场。数值方法中, 空间离散格式为中心差分, 用标量耗散模型抑制数值波动。用以经典四阶龙格-库塔法为基本迭代格式的时间推进方法求解控制方程组。电势的迭代计算采用多重网格加速收敛, 用隐式残值光滑技术改善收敛速度以及时间推进过程的稳定性。计算取得初步的成功: 电弧已经出现并可观察到电弧喷射器内的离解和电离状况以及化学不平衡、粘性等效应对流动过程的影响。 The internal flow field of an arcjet using nitrogen as working gas was simulated under the hypothesis of LTE.The flow model was the extended Navier Stokes equation system coupling with the electromagnetic field.The electric field was simulated by electric potential equation.A time stepping scheme using 4th order classical Rouge Kutta method was used to get the result.The electromagnetic field was calculated only in the first Rouge Kutta step and froze in the others,which can reduce the computational load while not affect the convergence characteristic.Other steps including multigrid techniques and residue smoothing were taken to accelerate the convergence rate and improve the calculation stability.The calculation is successful.The arc appear around the axis and characteristics of dissociation and ionization and other phenomenon such as the effects of chemical nonequilibrium and viscosity can be observed.
出处 《推进技术》 EI CAS CSCD 北大核心 1999年第6期52-57,共6页 Journal of Propulsion Technology
关键词 电弧喷射 数值仿真 等离子体射流 火箭发动机 Aarjet engine,Numerical simulation,Plasma jet,Flow distribution
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参考文献2

  • 1廖宏图,推进技术,1999年,20卷,4期
  • 2廖宏图,推进技术,1999年,20卷,5期

同被引文献38

  • 1肖应超,汤海滨.电弧喷射推力器化学非平衡数值模拟[J].推进技术,2004,25(5):458-462. 被引量:3
  • 2沈岩,赵文华,石泳,陈黎明.发射光谱测量电弧加热发动机羽流温度[J].推进技术,2005,26(1):72-75. 被引量:6
  • 3代玉杰,刘金远,王学慧.等离子体压强对Line-tied扭曲不稳定性增长率和本征函数的影响[J].核聚变与等离子体物理,2010,30(4):306-311. 被引量:9
  • 4马铁林,马东立,张华.大展弦比柔性机翼气动特性分析[J].北京航空航天大学学报,2007,33(7):781-784. 被引量:21
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  • 6John Slough, Ewing J J. Microarcjet microthruster for nanosat applications[ R]. A1AA 2007-5181.
  • 7Fife J M, Bromaghim D R, Chart D A, et al. Orbital per- formance measurements of air force electric propulsion space experiment ammonia arcjet[J]. J. Propulsion and Power, 2002, ! 8 ( 4 ) : 749-753.
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