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一个可以对任意长整数进行加减的类
- 在Visual C++6.0 WinXp下编译通过采用类来实现,从CString继承而来数据运算的结果保存在CString类中理论上可对任意长的数据进行相加在Release目录下有可执行文件，将*.txt拖放到longadd.exe上即可，*.txt为数据文件-in Visual C Compiler 6.0 WinXp adopted under the category achieved redeem inherited from the Operational data stored in
aiefoilconclution.rar
- 已知实验测得的翼型的压力分布和翼型数据，计算其升力系数和阻力阻力,Known experimental measured airfoil pressure distribution and airfoil data to calculate the lift coefficient and drag resistance
all
- 计算流体力学软件Fluent中所有的曳力模型UDF程序-Fluent CFD software, all of the drag model for UDF
Drag-Coefficient
- list of lift coefficeint and drag coefficient for naca 0012 at different reynolds No.
naca-0012-drag-prediction
- Drag prediction for Naca 0012 by use of different source codes and Compare with Experiment results.
Gidaspow
- fluent 多相流模型中的Gidaspow曳力模型，采用udf 编写。可以再fluent 中进行编译-Gidaspow drag law for multiphase flow in fluent in UDF scheme.
Dns-code
- 牛顿 非牛顿流体数值模拟源代码，对粘弹性流体湍流减阻进行分析-Newton non-Newtonian fluid numerical simulation of the source code, to analyze the viscoelastic fluid turbulent drag reduction
Airfoil
- 采用excel编写了翼型升力系数、阻力系数及力矩系数的360°扩展程序-Using excel to prepare the airfoil lift coefficient, drag coefficient and torque coefficient 360 extension
sdf
- 这是关于卫星运动考虑大气阻力时，重要参数大气阻力系数计算的文章，具体公式及方法都已给出-This is the atmospheric drag on satellite sports, the articles of the important parameters of atmospheric drag coefficient, specific formulas and methods have been given
TOEPLZ
- 拖布利兹矩阵的快速分解fortran程序，最近在搞地震数据处理，自己编程实现好多数值算法。-Rapid decomposition of the matrix drag Blitz fortran program, recently engaged in seismic data processing, a lot of their own programming numerical algorithms.
source-code
- 采用斜激波-膨胀波理论计算流场中对称菱形翼型各个表面的压力系数及翼型升阻力系数-Using oblique shock- expansion wave theory rhombus symmetrical airfoil flow field in each surface pressure coefficient and airfoil lift and drag coefficients
yeli
- 基于fluent手册改编的一个用于计算密相流化床的曳力模型-a drag model
zulixishu
- 使用插值法计算阻力系数，给出不同马赫数下的阻力系数，然后对给定马赫数进行插值-Drag coefficient is calculated using the interpolation method, the drag coefficient is given under different Mach number, and then interpolate a given Mach