搜索资源列表
特征线方法设计二维喷管
- tezhegnxian,特征线法计算二维激波管
isight_01
- 发动机喷管设计以及性能优化计算，由isight实现，bat批处理-the calculation for out
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
weipenguan
- 超高声速尾喷管的设计，手缩段是圆弧加直线前段设计。-Design of the super loud speed tail nozzle, the design of the circular arc and straight line.
nozzle
- 双圆弧喷管的型面设计。根据燃烧室的相关参数和喷管的背压可以设计出具有良好工作性能的双圆弧喷管，该喷管是基于特征线法的一种简化，方便加工。-Profile design of double circular nozzle. According to the relevant parameters of the combustion chamber and the nozzle back pressure can design of dou
Mocprog
- 用MOC（特征线法）方法设计喷管，把相应参数输入即可得到理想的型面。-The nozzle is designed with the MOC (feature line method) method, and the corresponding parameters can be input to obtain the ideal surface.
super_ellipse
- 采用超椭圆方程设计过渡段,主要针对风洞设计及喷管设计(The transition section is designed by using super-elliptic equation)
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)
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)
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.)
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)