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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, AUSMDV and AUSM+ are employed for this code. In order to improve the calculation accuracy, the MUSCL interpolation with various type limiter are used.)
- 2014-04-09 13:39:33下载
- 积分：1
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time_seris
时间序列预测算法。支持5种常见的算法
移动平均
非线性回归
指数平滑等(ar, ardemo ma)
- 2021-04-18 15:38:57下载
- 积分：1
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3
说明： 数值分析 显示算法 非线弹性 滞回曲线(Numerical analysis showed that the algorithm the linear elastic hysteresis curve)
- 2012-01-09 16:26:03下载
- 积分：1
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Vmodel
汽车仿真模型，包含七自由度仿真模型、m文件和数学方程式(Car simulation model，Contains seven degrees of freedom simulation model m file and mathematical equations)
- 2021-03-30 16:09:09下载
- 积分：1
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fsolve-function-nonlinear-equations
fsolve函数求非线性方程组数值解，已经验证其正确性。(fsolve function for the numerical solution of nonlinear equations)
- 2013-08-05 09:25:31下载
- 积分：1
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ansys2
【ansys基本建模算例】带法兰油缸的有限元分析，计算相关应力即变形([Examples] basic modeling ansys finite element analysis with flanged cylinder, calculating the stress that is associated deformation)
- 2014-05-04 20:39:30下载
- 积分：1
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bifurcation and LE
计算非线性系统的分叉图和李雅普诺夫指数，用于判断系统的混沌状态，独立的两个文件(a tool to calculate bifurcation and Lyapunov exponent)
- 2018-05-28 22:25:00下载
- 积分：1
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shiyan4
若矩阵A中的某一元素A[i，j]是第i行中的最小值，而又是第j列中的最大值，则称A[i，j]为矩阵A中的一个鞍点。请写出一个可确定此鞍点位置的算法（如果这个鞍点存在）。(If the matrix A, an element A [i, j] is the minimum value in the i-th row, but is the maximum value of the j-th column, then A [i, j] for the matrix A is a saddle point. Please write a algorithm to determine the position of saddle point (saddle point exists).)
- 2013-01-07 13:16:11下载
- 积分：1
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zoeppritz
这是用于求解精确求解zoeppritz方程的程序，可用于AVO反演，合成地震记录等(This function computes the particle displacement reflection and
transmission coefficients (the relative displacement amplitudes)
for a solid-solid interface, a liquid-solid interface,
a solid-liquid interface, and a liquid-liquid interface.
The medium on each side of a given interface is perfectly elastic.
The output is the value of the reflection or transmission
coefficient, specified by the user at the incidence angle anginc
(see input parameters).
)
- 2012-07-24 11:46:34下载
- 积分：1
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ftcs-code
fortran based code for 1d heat equation
- 2014-10-06 02:17:56下载
- 积分：1
