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Numerical Simulation of Hypersonic Flow Around an Aerospace Plane by Parallel RANS based CFD

机译：基于并行RANS的CFD数值模拟绕飞机飞行的超音速流

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Wang Chao; Li Feng; Ding Zhi-chao; Zhang Liang;
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年度 2013
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1. CFD prediction of fluid flow and mixing in stirred tanks: Numerical issues about the RANS simulations [J] . M. Coroneo, G. Montante, A. Paglianti, Computers & Chemical Engineering . 2011,第10期

机译：搅拌釜中流体流动和混合的CFD预测：关于RANS模拟的数值问题
2. Numerical investigation of an advanced U-RANS based pressure fluctuation model to simulate non-linear vibrations of nuclear fuel rods due to turbulent parallel-flow [J] . Kottapalli S., Shams A., Zuijlen A. H., Annals of nuclear energy . 2019,第JUNa期

机译：基于高级U-RANS的压力波动模型的数值研究，以模拟湍流平行流引起的核燃料棒的非线性振动
3. SIMULATION OF HYPERSONIC FLOWS USING THE QGD-BASED PARALLEL PROGRAM COMPLEX "EXPRESS-3D" [J] . Evgeny V. Shilnikov, Tatiana G. Elizarova High Temperature Material Processes . 2018,第2a3期

机译：基于QGD的并行程序复杂的“Express-3D”模拟超声波流量
4. Numerical simulation of hypersonic flow around an aerospace plane by parallel RANS based CFD [C] . Chao Wang, Feng Li, Zhi-chao Ding International Conference on Parallel Computational Fluid Dynamics . 2014

机译：基于CFD的平行rans rans rans围绕航空航天平面周围超声波流动的数值模拟
5. Parallel implicit algorithms for direct numerical simulations of hypersonic boundary layer stability and transition. [D] . Dong, Haibo. 2003

机译：用于高超声速边界层稳定性和跃迁直接数值模拟的并行隐式算法。
6. An adaptable parallel algorithm for the direct numerical simulation of incompressible turbulent flows using a Fourier spectral/hp element method and MPI virtual topologies [O] . A. Bolis, C.D. Cantwell, D. Moxey, -1

机译：使用傅里叶频谱/ hp元素方法和MPI虚拟拓扑对不可压缩湍流进行直接数值模拟的自适应并行算法
7. A Guidance to Grid Size Design for CFD Numerical Simulation of Hypersonic Flows [O] . Zhang H.R., Yu Y. 2013

机译：高超声速流CFD数值模拟的网格尺寸设计指南
8. Numerical Simulation of Hypersonic Aerodynamics and the Computational Needs for the Design of an Aerospace Plane. [R] . Liu, S. K. 1992

机译：高超声速空气动力学数值模拟及航空航天飞机设计的计算需求。

Numerical Simulation of Hypersonic Flow Around an Aerospace Plane by Parallel RANS based CFD

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