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kiva3
- 用于燃烧的frotran的插件源代码，用于燃烧分析颇有帮助-The plug-in for burning frotran source code, quite helpful for combustion analysis
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
soot
- The following is a list of codes available. Please consult the manual for details The present version of the codes is consistent (and was tested) with the Appel-Bockhorn-Frenklach gas-phase combustion mechanism. FORTRAN Soot Subroutine
normal.tar
- Numerical scheme for 1D normal premixed combustion based on Godunov scheme
coal-combustion-----simulation-
- 一个采用数值模拟来计算煤粉燃烧时各参数情况的经典算例，附件文件可直接用FLUENT打开，附件中并且有计算结果截图，供学习参考用-A numerical simulation to calculate the parameters of the classic case study during coal combustion, file attachments can be opened directly using FLUENT, and there annex calculations sc
CFD2013-12
- 中科院力学所张新亮老师的计算流体力学上课课件第12讲-燃烧的数值计算-Chinese Academy of Mechanics CFD school teacher Zhang Xinliang courseware Lecture 12- numerical combustion
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
flame
- 一个刚性常微分方程。 火焰（R0）指定初始半径R0。默认的R0 = 02。 一个火球会膨胀，直到它的半径足够大，所有的氧气都可以通过地表燃烧。半径的方程^ RDOT = R 2 R ^ 3。(A stiff ordinary differential equation. FLAME(r0) specifies the initial radius is r0. Default r0 = .02. A ball of fire grows until its radius is ju