搜索资源列表
nozzle
- 拟一维喷管流动的数值解fotron源程序， 跨声速
nozzle-fortran
- one dimension nozzle flow; fortan coding
charpt7_3
- 安德森《计算流体力学及其应用》第七章拟一维喷管流动的数值解 7.3节 亚声速—超声速等熵喷管流动的CFD解法 。-Anderson the computational fluid mechanics and its application "chapter 7 quasi one-dimensional nozzle flow numerical solution of section 7.3 subsonic- supersonic isentropic nozzle flow of
main
- 喷管内的结构网格生成，利用了好几种迭代方法-The structure of nozzle grid generation, use of several iterative method
nozzle
- 采用预报-校正格式的拟一维喷管流动的数值解法 -Quasi one-dimensional numerical solution of nozzle flow
ycpenguan
- 拟一维亚声速---超音速等熵喷管流动的CFD解法-Via the speed of sound to be a supersonic isentropic nozzle flow--- the CFD solution
lyg
- 一维喷管流动数值模拟的全超声速解法，与其他的有一些区别-One-dimensional numerical simulation of the entire nozzle flow supersonic solution, there are some differences with other
work
- 本人对拉瓦尔喷管进行流体分析，得出了其温度，压力等仿真曲线。内有程序和仿真图-I am Laval nozzle for fluid analysis, obtained the temperature, pressure and other simulation curve. There are procedures and simulation diagram
pressure-established
- 端面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，装药直径，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-Face charge calculation of solid rocket motor process of establishing the working pressure Input for the specific heat ratio, gas gas constant, ignition temperature,
tube-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，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-tube type of solid rocket motor combustion pressure build process calculation programs for heat input than, gas gas constant, the ignition temperature, propellan
1D-nozzle-flow
- 一维喷管流动，采用maccormack算法，对变量在时间空间维度进行计算-1D nozzle flow,maccormack
macmark_SCHME
- 高精度的马克 84显隐算法。采用了世通量分裂技术，算列是喷管问题-Precision Mark Mark 84 explicit-implicit algorithm. World flux splitting technique, count out the nozzle problem
nozzle-and-diffuser
- 模拟二维可压缩超音速风动内的流动参数随风动形状的变化-Simulate the two-dimensional compressible supersonic wind-driven flow parameters in the wind dynamic changes in shape
Macormack-solver
- 一维拉瓦尔喷管的CFD模拟，格式为Macormack-The Villa Val nozzle CFD simulation, the format is Macormack
quasi-1d-laval
- 准一维拉瓦尔喷管求解程序，MacCormack格式-Junichi Villa Val nozzle solver, MacCormack format
BEAM_WARMING_BOUNDARY_SET_1
- solve Euler equations in nozzle with Flux vector splitting method
CFD7_5
- 亚音速-超音速等熵喷管，守恒形式方程,MacCormack方法求解-Subsonic- supersonic isentropic nozzle, conservation equation form, MacCormack method for solving
for
- 采用离散的数值方法，通过坐标转换并生成贴体网格系统，计算轴对称喷管流场-Discrete numerical methods, through coordinate transformation and generate body-fitted grid system, calculating axisymmetric nozzle flow
Nozzle-simulation1
- 喷管模拟实例对应于入口亚音速出口超音速情形，欢迎下载，是在MIT访问期间的部分工作-Simulation of nozzle operating at the inlet sonic and outlet supersonic
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 double circular nozzle having a g