搜索资源列表
Matla_CFD
- 这几个算例都是MacCormack格式的,喷管计算用时间步进法,外突钝角绕流用空间步进法.都写成模块形式,便于查错. -these examples are MacCormack format, the nozzle calculation time stepping, fr a med obtuse angle with space bypass Step law. Modules are written form that fa
喷管中气体流动现象及参数测定
- penguan，喷管中气体流动
Matla_CFD
- 这几个算例都是MacCormack格式的,喷管计算用时间步进法,外突钝角绕流用空间步进法.都写成模块形式,便于查错. -these examples are MacCormack format, the nozzle calculation time stepping, fr a med obtuse angle with space bypass Step law. Modules are written form that fa
hw-nozzle
- 求解二维无粘欧拉方程，算的是一个二维收扩喷管-Solving two-dimensional inviscid Euler equations, operator of a collection of two-dimensional expansion nozzle
SteamFlow
- 可用于直接计算二维喷管中的湿蒸汽流动，输入初始条件，边界条那件和迭代次数和步长即可。-study on the wet steam flow with condensation in the laval nozzle ，with fortran code。
muscl
- 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
nozzle
- 国外经典二维喷管，matlab程序，相当经典-Nozzle matlab program
chapter7
- 该程序是约翰 D. 安德森（John D. Anderson）所著的《计算流体力学基础及其应用》（Computational Fluid Dynamics）第七章的拟一维喷管流动数值解的程序。(This code is developed to solve the quasi one dimensional nozzle flow problem in the Chapter 7 of Computational Fluid Dynam
1-D 欧拉（Euler）方程求解Laval缩放喷管.rar
- 参照Blazek博士的单元节点法准1-D 欧拉（Euler）方程程序，编写采用单元中心法的准1-D 欧拉（Euler）方程求解Laval缩放喷管的程序。(Referring to Dr. Blazek's element node method, the quasi 1-D Euler equation procedure is used to prepare the quasi 1-D Euler equation using th
拟一维喷管流动的数值解
- 拟一维喷管流动的数值解，采用尼克森法求解喷管内的流动(Numerical solution of quasi one dimensional nozzle flow)
nozzle_design
- 主要针对新一代战斗机尾喷管的复杂型面设计，型面变化设计(The design of profile change for the new generation of fighter nozzle is very important)
python
- 亚声速-超声速等熵喷管流动的CFD解法，运用python语言对方程的求解实现。(CFD solution for the flow of subsonic and supersonic isentropic nozzle,the solution of the equation is realized by using the python language.)
nozzle_flow7_3
- 一维喷管流动,亚声速—超声速等熵喷管流动的CFD解法(nozzle flow,A CFD Solution to the Velocity of Subsonic Velocity-Sonic Isothermal Nozzles)
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)
拟一维喷管流动的数值解法(MATLAB)代码
- MacCormack差分格式进行求解变截面喷管流动(MacCormack difference scheme for variable cross-section nozzle flow)
NozzleDesign-master
- NASA的超声速喷管设计程序，包含有气体数据库，功能强大(NASA's supersonic nozzle design program, including a gas database, is powerful)
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.)
niyiweipenguan
- matlab软件用maccormack方法编写拟一维喷管的程序(Matlab software uses MacCormack method to program quasi one dimensional nozzle)
ccb07eb6f839a9af2949a7290738cc95-1
- 实现喷管的参数化设计，对其进行相关参数的影响性分析(The parametric design of nozzle is realized, and the influence of related parameters is analyzed)
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)