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喷头流量系数计算程序
- 喷头流量系数计算程序,自己编的一个小程序，但对搞节水灌溉的很适用哦-nozzle flow coefficient calculation procedures, their own small part of a process, but to engage in water-saving irrigation is applicable oh
star-charge-pressure-established
- 管型燃烧固体火箭发动机压强建立过程计算程序 输入为比热比，燃气气体常数，点火温度，推进剂密度，星角数，星角度大小，装药直径（内径和外径），喷管喉部直径，装药体积，燃速相关常数 输出为压强和工作时间-Star of solid rocket motor combustion pressure build process calculation programs for heat input than, gas gas constant, the ignition temperature, prop
nozzle
- 电子书籍《AndersonJ.D.-Computationalfluiddynamics》的第七章源程序。-E-books
yiwei
- 拟一维喷管流动的数值解，约翰D.安德森书上第7章内容，自编-Quasi one-dimensional numerical solution of nozzle flow
Nozzles
- nozzle flow descr iption. Explaining different types of nozzle used in thrust enhancement.
nozzle
- 拟一维喷管流动的数值模拟程序，FORTRAN版本-Quasi one-dimensional nozzle flow simulation program, FORTRAN version
unsteady_compressible
- fluent中压力入口的udf，一个喷嘴的源码-fluent udf, pressure on the entrance to a nozzle source
aa
- 计算火箭发动机推力室的喷气速度随喷管压强比和喷管面积比变化的规律-Jet speed calculation rocket engine thrust chamber with the nozzle pressure ratio and nozzle area ratio changes in the law
earth_particle
- c#采用sharpgl显示地球、飞行器以及粒子流，通过键盘WSADQE控制视景的观展角度，通过1234控制四个喷管粒子的喷射。-c# using sharpgl show the Earth, spacecraft and particle flow, controlled by the keyboard WSADQE visual angle of view of development, by 1234 the four control injection nozzle particles.
Nozzle-testing
- 注塑成型喷嘴检测实例，halcon成功的例子-Injection molding nozzle detection example, halcon successful examples
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.
Rao-nozzzle-design
- 对Rao喷嘴进行了设计，并输出图形 数据-design of Rao nozzle and output figure
Conical-nozzle-design
- 本程序对Conical喷嘴进行了设计，并输出图形和数据-This program was designed to Conical nozzles and output data and graphics
MATLAB
- 计算流体力学准以为喷管流动的数值解，是自己编的小程序。-Numerical Solution Nozzle Flow CFD quasi-think their own series of small programs.
CFD-7
- 对应计算流体力学基础及应用中第7章中的例子，有助于读者学习喷管内流场的分布，为深入学习计算流体力学打下坚实的基础(Corresponding to the basis of computational fluid dynamics and the examples in the seventh chapter, it will help readers to study the distribution of the flow field in the nozzle, and lay a sol
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 Dynamics writen by John D. Anderson
Handouts
- 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。(According to the procedure of Euler equation of the unit node of Dr Blazek, the procedure of using the quasi-1-d Euler (Euler) equation of the unit central method to solve t
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)
Area_Mach_relation
- 一个普通的具有收缩和放大的喷嘴设计模型, 用matlab编写完成(A design of a convergent & divergent nozzle)