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气动激光器喷管非平衡流2维数值仿真 被引量:1

2D numerical simulation for non-equilibrium flow in gasdynamic laser nozzle
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摘要 将Anderson的两振型三温度弛豫模型和严海星整理的弛豫数据相结合,采用2维守恒型方程组对按照最小长度喷管型面设计方法设计的、面积比分别为50和20的气动激光器喷管非平衡流场进行了数值仿真。小信号增益计算结果在每个计算点都和J.S.Vamos等人针对这两种喷管的小信号增益测量试验结果符合很好.解决了传统的准1维非平衡流分析方法不能很好地和试验结果相符的问题.对气动激光器喷管性能设计提供了更精确的评估方法。 Anderson's relaxation model of two modes and three vibrational temperatures was combined with Yan Haixing's vibrational relaxation data to simulate 2D non-equilibrium nozzle flows in a gasdynamic laser.Two different minimum-length nozzles with supersonic area ratios of 50∶1 and 20∶1 were studied by numerically solving the conservational equations.The small signal gains of the simulation results agree very well with J.S.Vamos's experiments for both nozzles.This analysis method solves the problem of matching the non-equilibrium nozzle flow analysis results of gasdynamic laser nozzles with the experimental data,which conventional quasi-one-dimensional simulation cannot do well.By this way,highly accurate method of evaluating a gasdynamic laser nozzle's performance was realized.
出处 《强激光与粒子束》 EI CAS CSCD 北大核心 2010年第5期959-962,共4页 High Power Laser and Particle Beams
基金 国家部委基金资助课题
关键词 气动激光器 小信号增益 非平衡流场 数值仿真 gasdynamic laser small signal gain non-equilibrium nozzle flow numerical simulation
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参考文献11

  • 1严海星 陈丽吟.气动激光器的非平衡流计算.力学学报,1978,10(4):274-287.
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  • 3李树山.CO2-N2-H2O激光体系弛豫方程的分类及其增益计算比较.中国激光,1979,(7):10-18.
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二级参考文献1

  • 1严海星,力学学报,1978年,4期,274页

共引文献3

同被引文献6

  • 1严海星 陈丽吟.气动激光器的非平衡流计算.力学学报,1978,10(4):274-287.
  • 2Dumitrescu L Z. Minimum length axisymmetric laval nozzles[J]. AIAA Journal, 1975, 13(4)..520-531.
  • 3邬传保 俞刚.气动激光器列阵喷管的研究.中国激光,1980,:21-26.
  • 4Sauer R. Method of characteristics for three-dimensional axially symmetrical supersonic flows[R]. NACA, 1947.
  • 5李树山.c02一N2-H20激光体系弛豫方程的分类及其增益计算比较.中国激光,1979,:10-18.
  • 6严海星.COz-N2-H20激光体系的振动弛豫过程速率数据.中国激光,1981,:1-8.

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