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Description: 有限体积法求解一维欧拉方程，采用二阶MUSCL迎风格式，计算一维等熵喷管的流程，喷管扩张段有正激波。有助于理解和学习MUSCL格式
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Size: 2200 |
Author: 李超 |
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Description: C语言实现二维无粘欧拉方程的求解，采用二阶迎风MUSCL格式，求解二维收扩喷管，计算时间比MATLAB少很多
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Size: 46557 |
Author: 李超 |
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Description: 用FORTRAN语言实现二维欧拉方程的求解，采用二阶MUSCL迎风格式
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Size: 258150 |
Author: 李超 |
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Description: 有限体积法求解一维欧拉方程，采用二阶MUSCL迎风格式，计算一维等熵喷管的流程，喷管扩张段有正激波。有助于理解和学习MUSCL格式
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Size: 2048 |
Author: 李超 |
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Description: C语言实现二维无粘欧拉方程的求解，采用二阶迎风MUSCL格式，求解二维收扩喷管，计算时间比MATLAB少很多-C Language Implementation of two-dimensional inviscid Euler equations, using second-order upwind MUSCL format, solving two-dimensional expansion nozzle closed, the computation time much less than the MATLAB
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Size: 265216 |
Author: 李超 |
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Description: 用FORTRAN语言实现二维欧拉方程的求解，采用二阶MUSCL迎风格式
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Size: 570368 |
Author: 李超 |
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Description: Muscl Euler Two dimensions
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Size: 139264 |
Author: huangjx |
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Description: 基于muscl格式一维喷管流动计算，格式采用参数η取为0 的Van Leer限量因子。-muscl
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Size: 1024 |
Author: ygy |
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Description: Toro的slic方法的一维浅水程序，蚕蛹muscl重构-Program name: HW-SLIC
File name: hw_slic.f
Purpose:
To solve the time-dependent non-linear one dimensional shallow water equations by the SLIC method. The method involves a MUSCL reconstruction of the data, time evolution of the boundary extrapolated values followed by application of the first-order centred FORCE flux
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Size: 5120 |
Author: 周润发 |
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Description: 做浅水计算的都知道TORO什么概念， 这是他老先生的muscl-hancock加h-Program name: HW-MUSH
File name: hw_mush.f
Purpose:
To solve the time-dependent non-linear one dimensional shallow water equations by the MUSCL-Hancock method in conjunction with the HLL approximate Riemann solver
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Size: 5120 |
Author: 周润发 |
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Description: 用Roe格式求解黎曼激波管问题的Fortran源代码。可以通过MUSCL插值来提高求解精度。适合计算流体力学的初学者参考学习。-Riemann shock tube problem with Roe scheme. You cam improve the accuracy by MUSCL interpolation. This code is suitable for CFD beginners.
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Size: 2048 |
Author: 王逗 |
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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: Solving 2D Euler equations by MUSCL interpolation for contact discontinuities
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Size: 10240 |
Author: planck |
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Description: 一、通过数值求解Euler方程，模拟一维激波管算例，lax shock tube算例，interaction blast wave算例，Shu-orsher算例，low density算例。
二、其中采用的数值格式有：一阶迎风格式, 三阶迎风格式, 2、3、4阶MUSCL格式, 3、5、7阶WENO格式。(First, by numerical solution of the Euler equation, the simulation of one-dimensional shock tube example, lax, shock, tube example, interaction, blast, wave example, Shu-orsher example, low density example.
Two. The numerical schemes used include: first order upwind scheme, three order upwind scheme, 2, 3, and 4 order MUSCL schemes, 3, 5, and 7 order WENO schemes.)
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Size: 15360 |
Author: hsqkk
|
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Description: 本程序用于求解一维无粘可压缩欧拉方程（激波管问题）
运用Dummy Cell处理边界条件;
通量计算方式: AUSM Scheme;
重构方法：MUSCL方法
限制器：Van Albada限制器
时间离散：四步Runge-Kutta方法(his program is used to solve one dimensional inviscid compressible Euler equation (shock tube problem) Application Dummy Cell Treatment of boundary conditions ; Flux calculation method AUSM Scheme; Refactoring method: MUSCL Method Limiter: Van Albada limiter Time discretization: four steps Runge-Kutta Method)
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Size: 13312 |
Author: cfdzaza |
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