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[Other resource] ausm DL : 0: 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
Update : 2008-10-13 Size : 2.37kb Publisher : 杨佳庆
[Algorithm] ausm DL : 1: 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
Update : 2025-02-17 Size : 2kb Publisher : 杨佳庆
[Mathimatics-Numerical algorithms] EULERAUSM DL : 2: 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
Update : 2025-02-17 Size : 450kb Publisher : 袁振伟
[Mathimatics-Numerical algorithms] AUSM DL : 0: C++语言AUSM+格式，有限体积法，注释也不是太多-C-AUSM+ format, finite volume method
Update : 2025-02-17 Size : 1kb Publisher : 钱云
[Mathimatics-Numerical algorithms] SIMPLER20B3CCD0F_1211121594 DL : 0: 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,
Update : 2025-02-17 Size : 140kb Publisher : 钱云
[Mathimatics-Numerical algorithms] CFDroe DL : 0: 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
Update : 2025-02-17 Size : 89kb Publisher : 钱云
[Algorithm] naca0012 DL : 0: NACA0012翼型流场计算。结构化网格，AUSM格式。-NACA0012 airfoil flow field
Update : 2025-02-17 Size : 584kb Publisher : newanda
[Communication-Mobile] ausm-euler0012 DL : 0: this fortran code can be used for analyse Inviscid flow over naca0012 airfoil with C_type grid. this code is developed by AUSM+ method.
Update : 2025-02-17 Size : 3kb Publisher : kiarash
[Algorithm] A-solver-for-1-D-RIEMANN-problem DL : 0: 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.
Update : 2025-02-17 Size : 107kb Publisher : 倪奇峰
[Algorithm] ausm DL : 0: AUSM FOR THE CFD SOLVER
Update : 2025-02-17 Size : 2kb Publisher : BUDAK
[Other] AUSM DL : 1: 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
Update : 2025-02-17 Size : 966kb Publisher : 孙阳
[matlab] AUSM-FOR-CIRCULAR-BODY-FLOW DL : 0: AUSM求解半圆面NS方程(海平面参数)-AUSM METHOD FOR CIRCULAR BODY FLOW WITH SEA-LEVEL CONDITION
Update : 2025-02-17 Size : 2.3mb Publisher : 陈烨
[source in ebook] AUSM DL : 0: 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)
Update : 2025-02-17 Size : 6kb Publisher : dengli
[Other] shock-tube-for-Ausm DL : 0: 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
Update : 2025-02-17 Size : 6.66mb Publisher : 王园丁
[Algorithm] CFD DL : 0: 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.
Update : 2025-02-17 Size : 7kb Publisher : 王逗
[transportation applications] AUSM_MUSCL DL : 1: 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
Update : 2025-02-17 Size : 726kb Publisher : 吴新民
[Industry research] analyze-and-compare- DL : 0: 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.
Update : 2025-02-17 Size : 834kb Publisher : 柏安翔
[Graph program] mvsjgg DL : 0: 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()
Update : 2025-02-17 Size : 452kb Publisher : lqi@87480
[Mathimatics-Numerical algorithms] liou_steffen DL : 0: 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.)
Update : 2025-02-17 Size : 1kb Publisher : bread31
[Other] ausm DL : 1: 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)
Update : 2025-02-17 Size : 3kb Publisher : 212121dear

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