搜索资源列表
ausm
- 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
AUSM
- C++语言AUSM+格式,有限体积法,注释也不是太多-C-AUSM+ format, finite volume method
naca0012
- NACA0012翼型流场计算。结构化网格,AUSM格式。-NACA0012 airfoil flow field
CFDroe
- 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
EULERAUSM
- 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
SIMPLER20B3CCD0F_1211121594
- 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,
A-solver-for-1-D-RIEMANN-problem
- 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 t
ausm
- AUSM FOR THE CFD SOLVER
AUSM-FOR-CIRCULAR-BODY-FLOW
- AUSM求解半圆面NS方程(海平面参数)-AUSM METHOD FOR CIRCULAR BODY FLOW WITH SEA-LEVEL CONDITION
CFD
- 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,
oned_euler_fluxes_v5
- 一维欧拉方程计算,集合了Lax-Friedrichs,Richtmyer,MacCormack,Steger-Warming,Van Leer,AUSM,Zha-Bilgen,Godunov,Osher,Roe,Rusanov,HLL(HLLE),HLLL,AUFS方法(One dimensional Euler equation, including Lax-Friedrichs, Richtmyer, MacCormack, Steger-Warming, Van Leer, AUSM, Z
aaduqf1
- 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()
liou_steffen
- 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.)
新型上风格式_AUSM_的性能分析及其应用_陈靓
- 研究了新型上风格式AUSM+的分辨率、效率等性能,并用它与Roe、van Leer上风格式数值模拟了前向台阶激波反射流动,通过对激波、膨胀波、接触间断及其间相互干扰的复杂波系的模拟对比,分析探讨了AUSM+格式的低数值耗散、间断高分辨率等特性。(The resolution and efficiency of the new upwind scheme AUSM+ are studied, and the flow of forward step shock wave is simulated