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Here is a 1D Euler code (1D shock tube code) for solving Sod s shock tube
problem, using Roe s Approximate Riemann solver, minmod limiter, and 2-
stage Runge-Kutta time-stepping. Learn how a second-order non-oscillatory
Euler code is written,
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一维 问题，即激波管问题，是一个典型的一维可压缩无黏气体动力学问题，并有 解析解。对它采用二阶精度 两步差分格式进行数值求解。-One-dimensional problem, namely shock tube problem is a typical one-dimensional compressible inviscid gas dynamics problems, and analytical solutions. It uses a two-step difference schem
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This the fortran program for simulating a shock tube problem-This is the fortran program for simulating a shock tube problem
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一维欧拉方法的计算，解决Sod s激波管问题，使用李曼近似解-A method of calculating Viola, Sod' s shock tube problem solving, using Lehman approximate solution
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1d roe solver uses for shock tube problem and nozzle problem
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利用MacCormack差分格式求解一维激波管问题（Fortran77 语言版本）-Use MacCormack Difference Scheme for Solving the one-dimensional shock tube problem (Fortran77 language version)
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激波管问题是一个典型的一维可压缩无黏气体动力学问题，有解析解。对它采用二阶精度两步差分格式进行数值求解。这里给出了计算程序-Shock tube problem is a typical one-dimensional compressible inviscid gas dynamics problem, there are analytical solution. It uses a two-step difference scheme of second order accuracy num
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一维激波管问题数值计算，Lax格式和Jameson中心差分格式，激波间断的扑捉，输出结果用tecplot打开。-A one-dimensional numerical calculation shock tube problem, Lax scheme and Jameson central scheme, intermittent shock capture, output with tecplot open.
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求解欧拉方程一维激波管问题，quick格式和123阶迎风格式-Solving Euler Square One- dimensional shock tube problem, quick format, and 123 order upwind scheme
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采用多种黎曼求解器求解激波管问题，工况设计参照TORO的书，用C++编写-one dimensioal shock tube problem using a variety of Riemann solvers
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采用matlab编写，HLL和ROE黎曼求解器求解一维激波管问题，并有与精确黎曼求解器结果对比。-
one-dimensional shock tube problem using HLL and ROE Riemann solver
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此程序是中心格式，称作K-T格式（Kurganov-Tadmor）用于解决流体力学中一维激波管问题，例如sod问题等等。-CFD,central scheme(K-T格式)，1-D shock-tube problem，sod problem
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本程序用以解决流体力学中2维激波管问题，采用的计算格式有SHUS（simple high-order upwind scheme） 格式和van-Leer格式-CFD,2-D shock-tube problem,simple high-order scheme(SHUS),van-Leer scheme.
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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
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利用Lax-wendroff两步差分格式求解一维激波管问题Fortran语言-Use a two-step Lax-wendroff Difference Scheme for Solving the one-dimensional shock tube problem Fortran language
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一维 问题，即激波管问题，是一个典型的一维可压缩无黏气体动力学问题，并有 解析解。对它采用二阶精度 两步差分格式进行数值求解。-A one-dimensional problem that the shock tube problem is a typical one-dimensional inviscid compressible gas dynamics, and analytical solutions. It uses a two-step second order accuracy
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一维Euler方程求解，例子是激波管问题。采用了Godunov格式-one dimensional Euler equation solving for shock tube problem
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流体力学sod激波管问题的vanleer分裂，适合初学者使用。-Fluid mechanics sod shock tube problem vanleer division, suitable for beginners use.
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F语言编程解决一维激波管问题，本程序为精确解。(One dimensional shock tube problem in F programming)
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Fortran语言解决一维激波管问题，本程序为一阶迎风Roe格式(Fortran language to solve one-dimensional shock tube problem, this program is the first order upwind Roe format)
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