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Description: 一维热传导方程是最简单的偏微分方程，可供CFD初学者学习和参考
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Size: 2425 |
Author: 杨佳庆 |
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Description: 一维热传导方程是最简单的偏微分方程，可供CFD初学者学习和参考-One-dimensional heat conduction equation is the simplest partial differential equations for the CFD study and reference for beginners
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Size: 2048 |
Author: 杨佳庆 |
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Description: 基于ausm格式的欧拉方程求解程序，附带有naca0012的翼型数据，是学习计算流体力学的好例程，费尽心思编写的，注释多多，便于阅读-Ausm format based on the Euler equation procedures, comes with naca0012 the airfoil data, computational fluid dynamics is a good learning routines, the effort to prepare, notes a lot of easy-to-read
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Size: 460800 |
Author: 袁振伟 |
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Description: C++语言AUSM+格式，有限体积法，注释也不是太多-C-AUSM+ format, finite volume method
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Size: 1024 |
Author: 钱云 |
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Description: C++语言编写，基于有限体积法的AUSM+格式，-C++ language, based on the finite volume method of the AUSM+ format,
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Size: 143360 |
Author: 钱云 |
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Description: CFD，基于有限体积法的，Roe以及AUSM+up格式的C语言程序-CFD, based on the finite volume method, Roe and AUSM+ up format of C language program
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Size: 91136 |
Author: 钱云 |
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Description: NACA0012翼型流场计算。结构化网格，AUSM格式。-NACA0012 airfoil flow field
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Size: 598016 |
Author: newanda |
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Description: this fortran code can be used for analyse Inviscid flow over naca0012 airfoil with C_type grid. this code is developed by AUSM+ method.
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Size: 3072 |
Author: kiarash |
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Description: 分别采用Roe格式和AUSM格式求解一维黎曼问题，并将计算结果与解析解进行比较，发现这两种计算格式都能获得高的计算精度。-Roe scheme were used in this procedure and AUSM format to solve a 1-D RIEMANN problem, and numerical results were compared with the analytical solution, the results can be seen from these two formats have a solution with high accuracy.
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Size: 109568 |
Author: 倪奇峰 |
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Description: AUSM FOR THE CFD SOLVER
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Size: 2048 |
Author: BUDAK |
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Description: 完成前台阶问题的计算，利用的AUSMPW格式，算法结构较为简单，所以文字说明较少-Completed on the front steps of the calculation, use of AUSMPW format, the algorithm structure is relatively simple, so less text
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Size: 989184 |
Author: 孙阳 |
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Description: AUSM求解半圆面NS方程(海平面参数)-AUSM METHOD FOR CIRCULAR BODY FLOW WITH SEA-LEVEL CONDITION
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Size: 2414592 |
Author: 陈烨 |
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Description: 一个矩形计算域中有一个圆形区域，圆形区域内的充满高压气体，计算域其他地方压强较低，当薄膜破裂，将会形成激波（欧拉方程编写）-A rectangular computational domain of a circular area, circular area filled with high-pressure gas within the computational domain elsewhere low pressure, when the film rupture, will form shock (Euler equation written)
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Size: 6144 |
Author: dengli |
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Description: 激波管程序,AUSM数值计算格式，计算结果良好，是一个不错的CFD程序-shock tube program
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Size: 6986752 |
Author: 王园丁 |
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Description: 这是一个求解NACA0012翼型在不同马赫数与攻角下的流场的Fortran源代码。计算格式采用了原始AUSM、AUSMDV以及AUSM+格式。为了提高计算精度，使用了不同限制器的MUSCL插值。-This is a Fortran source code for solving the flow field around the NACA0012 airfoil at different Mach numbers and angles of attack. The scheme of AUSM, AUSMDV and AUSM+ are employed for this code. In order to improve the calculation accuracy, the MUSCL interpolation with various type limiter are used.
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Size: 7168 |
Author: 王逗 |
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Description: 计算流体力学中经典的AUSM-MUSCL格式的源程序。-code of ausm-muscl scheme by fortran
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Size: 743424 |
Author: 吴新民 |
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Description: 一维激波管问题差分格式计算对比分析，采用了MacCormack, Jameson, FVS, FDS, AUSM 的格式对一维激波问题进行分析计算，并对比了其性能-The comparison and analysis of one-dimensional shock tube problem with difference scheme is carried out. MacCormack, Jameson, FVS, FDS and AUSM are used to analyze and calculate the one-dimensional shock problem.
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Size: 854016 |
Author: 柏安翔 |
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Description: 基于ausm格式的欧拉方程求解程序,附带有naca0012的翼型数据,是学习计算流体力学的好例程,费尽心思编写的,注释多多()
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Size: 462848 |
Author: lqi@87480
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Description: 用于计算流体力学一维激波管问题计算的Fortran程序，分裂方法为AUSM(For the calculation of the 1D SOD tube problem, and the splitting method is AUSM.)
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Size: 1024 |
Author: bread31 |
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Description: 利用AUSM格式来求解欧拉方程,对NACA0012翼型进行流场求解,生成结构化网格(solve euler equation by the method of AUSM,and grid generation is done with structed grid)
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Size: 3072 |
Author: 212121dear |
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