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轴对称超临界粘性喷流的数值模拟
崔杰, 董松野, 张宝生
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,利用时间相关法,采用隐式的BeamWarming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。通过对超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:  纳维尔-斯托克斯方程  喷管气流  湍流射流  流动分布  数值模拟  数值计算
DOI:
分类号:V211.3
基金项目:
NUMERICAL SIMULATION OF AXISYMMETRICAL SUPERCRITICAL VISCOUS NOZZLE JET FLOW
Cui Jie, Dong Songye, Zhang Baosheng
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.
Key words:  Navier-Stokes equation  Nozzle gas flow  Turbulent jet  Flow distribution  Numerical simulation  Numerical calculation