Simulation of Flow over the ONERA M6 Wing Using a Parallel Implementation of an Implicit Scheme

V. E. Borisov

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Simulation of Flow over the ONERA M6 Wing Using a Parallel Implementation of an Implicit Scheme

机译：使用隐式方案的并行实现模拟ONERA M6机翼上的流动

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The flow over the ONERA M6 wing is numerically simulated using a parallel implementation of an implicit scheme with a third-order spatial approximation for the three-dimensional Reynolds-averaged Navier-Stokes equations based on the Spalart-Allmaras turbulence model modified by Edwards. The scalability of this parallel implementation is studied. The numerical results obtained are compared with experimental data and with the results obtained using an explicit scheme.

机译：使用基于爱德华兹修改的Spalart-Allmaras湍流模型的三维雷诺平均Navier-Stokes方程的三阶空间近似的隐式方案的并行实现，对ONERA M6机翼上的流动进行数值模拟。研究了这种并行实现的可伸缩性。将获得的数值结果与实验数据以及使用显式方案获得的结果进行比较。

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《Moscow University Mechanics Bulletin》 |2015年第4期|97-100|共4页
作者
V. E. Borisov;
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Moscow State University, Faculty of Mechanics and Mathematics, Leninskie Gory, Moscow, 119899, Russia;

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专利

1. A CASE STUDY IN PARALLEL COMPUTATION: VISCOUS FLOW AROUND AN ONERA M6 WING [J] . Zdenek Johan, Kapil K. Mathur, S. Lennart Johnsson, International Journal for Numerical Methods in Fluids . 1995,第10期

机译：并行计算的案例研究：ONERA M6机翼周围的粘性流动
2. Verification of Anisotropic Mesh Adaptation for Turbulent Simulations over ONERA M6 Wing [J] . AIAA Journal . 2020,第4期

机译：验证ONERA M6机翼上湍流模拟的各向异性网格自适应
3. Transonic Flow of Moist Air around the ONERA M6 Wing with Non-equilibrium and Homogeneous Condensation [J] . Sun Xiuling, Li Liang, Li Guojun Research journal of applied science, engineering and technology . 2013,第10期

机译：非平衡且均匀凝结的ONERA M6机翼周围潮湿空气的跨音速流动
4. Simulation of ONERA M6 Wing Flows for Assessment of Turbulence Modeling Capabilities [C] . Ricardo G. da Silva, Joao Luiz F. Azevedo, Edson Basso AIAA aerospace sciences meeting;AIAA SciTech Forum . 2016

机译：用于评估湍流建模能力的ONERA M6机翼流动的仿真
5. An implicit compact scheme solver for modeling steady-state and time-dependent axisymmetric flows with application to laminar diffusion flame simulations. [D] . Noskov, Mikhail. 2003

机译：一种隐式紧凑型方案求解器，用于建模稳态和时间相关的轴对称流，并将其应用于层流扩散火焰模拟。
6. Semi-implicit Non-conforming Finite-Element Schemes for Cardiac Electrophysiology: A Framework for Mesh-Coarsening Heart Simulations [O] . Javiera Jilberto, Daniel E. Hurtado -1

机译：心脏电生理的半隐式非协调有限元方案：网格粗化心脏模拟的框架
7. Comparison of RANS, DES and DDES Results for ONERA M-6 Wing at Transonic Flow Speed Using an In-House Parallel Code [O] . Durrani N., Qin N. 2011

机译：使用内部并行代码比较ONERa m-6机翼在跨音速流速下的RaNs，DEs和DDEs结果
8. Runge-Kutta Finite-Volume Simulation of Laminar Transonic Flow over the ONERA M6 Wing Using the Navier-Stokes Equations [R] . Muller, B., Rizzi, A. 1987

机译：利用Navier-stokes方程对ONERa m6机翼上层流跨音速流的Runge-Kutta有限体积模拟

Simulation of Flow over the ONERA M6 Wing Using a Parallel Implementation of an Implicit Scheme

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