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轴对称超临界粘性喷流的数值模拟
引用本文:崔杰,董松野,张宝生.轴对称超临界粘性喷流的数值模拟[J].推进技术,1994,15(3):14-20.
作者姓名:崔杰  董松野  张宝生
作者单位:航天工业总公司31所
摘    要:从雷诺平均的非定常Navier-Stokes方程出发,采用隐式的Beam-Warming格式中的矢通量分裂技术,结合Baldwin-Lomax代数湍流模型,数值模拟了收敛喷管的内流场和喷射流场,通过对趋临界工况下喷管跨音速流场的数值计算,表明本文的结果与试验结果是吻合的。

关 键 词:喷管气流  湍流射流  数值模拟

NUMERICAL SIMULATION OF AXISYMMETRICAL SUPERCRITICAL VISCOUS NOZZLE JET FLOW
Cui Jie,Dong Songye and Zhang Baosheng.NUMERICAL SIMULATION OF AXISYMMETRICAL SUPERCRITICAL VISCOUS NOZZLE JET FLOW[J].Journal of Propulsion Technology,1994,15(3):14-20.
Authors:Cui Jie  Dong Songye and Zhang Baosheng
Institution:The 31st Research Institute, Beijing, 100074;The 31st Research Institute, Beijing, 100074;The 31st Research Institute, Beijing, 100074
Abstract:The internal flow field and the flow jet field in a convergent nozzle are simulated based on Renolds-average unsteady Navier-Stokes equations, with time-dependent method, flux vector splitting technique in implicit Beam-Warming scheme and Baldwin-Lomax algebraical turbulent model. A transonic flow field in a nozzle under supercritical operation condition is numerically computated, which demonstrates that the results in this paper are in good agreement with experimental data.
Keywords:Navier-Stokes equation  Nozzle gas flow  Turbulent jet  Flow distribution  Numerical simulation  Numerical calculation  
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