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23_482
- 一维喷管流场计算FORTRAN语言编写无解压密码-one-dimensional nozzle flow calculation FORTRAN language without extracting passwords
nozzle
- 运载火箭用拉瓦尔喷管计算（此程序参数保密，仅上传源码供大家参考）
nozzle-shock
- 对拟一维喷灌流动的数值解的激波捕捉fortran源程
Test2 本程序调用Gambit自动生成喷管网格
- 本程序调用Gambit自动生成喷管网格，便于导入Fluent进行流场计算。程序中用到了从Cedit派生出的自定义类，适合本程序的方便使用。-This procedure is called Gambit nozzle automatically generated mesh into Fluent for easy flow field. The procedures used in the Cedit derived from a custom class for this program e
usjet
- 一份完整的通过USB端口通讯的可控单喷头应用文档，主要内容是用C++开发一个OCX控件，可以接收字符串和控制命令，转换为位图后传送给硬件喷印，付有详细说明文件。-Through the USB port of a complete single-nozzle application of the controllable communications documents, the main content is to develop a C++ OCX control that can rece
cuta
- 自己编写的关于计算一维喷管不可压流动数值解的fortran语言-I have written on the calculation of one-dimensional numerical solution of incompressible flow nozzle of the fortran language
code-for-Laval-Nozzle
- 拉瓦尔喷管内流场计算程序 用户可自行修改喷管型线A(x),进口总压、总温。给定出口静压后即可计算出喷管内流场压力、温度、速度、马赫数等物理参量的分布-code for the calculation of the flow field of the laval nozzel
214e41509b777d6a
- 特征线法设计二维轴对称喷管，采用MATLAB进行的喷管设计方法-nozzle design
pipe
- 模拟一维喷管流动的数值解，采用二位数组进行求解-Simulation of one-dimensional nozzle flow numerical solution using two-digit groups to solve
激波管
- 一维激波管的计算流体力学数值仿真计算，采用MacCormack法(Using MacCormack method to solve the problem of shock nozzle in MATLAB)
二维喷管的设计
- 二维喷管的设计，内含四个m文件。好不容易找到的。(Design of two-dimensional nozzle)
Console1
- 喷管射流传热程序测试，能够满足不同边界条件，能直接运行(The nozzle heat transfer program can satisfy different boundary conditions and run directly.)
Moc.java
- NASA的喷管设计程序，采用特征线方法，JAVA设计语言。(A Java Application to perform two dimensional analysis of supersonic flow through nozzles using the method of characteristics.)
拟一维喷管流动MacCormack法
- 计算流体力学CFD中的拟一维喷管流动，使用MacCormack迭代(The quasi one dimensional nozzle flow in CFD is solved by MacCormack iteration)