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: |
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NUMERICAL SIMULATION OF AXISYMMETRICAL SUPERCRITICAL VISCOUS NOZZLE JET FLOW |
Cui Jie, Dong Songye, Zhang Baosheng
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The 31st Research Institute, Beijing, 100074
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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 |