Title:
star-charge-pressure-established
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Description: Star of solid rocket motor combustion pressure build process calculation programs for heat input than, gas gas constant, the ignition temperature, propellant density, star Angle number, star Angle size, charging diameter (inside and outside), nozzle throat diameter, charging volume, burning rate pressure and related constant output to work time
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File list (Check if you may need any files):
xxl-xing\Debug\DF60.PDB
........\.....\xxl111.exe
........\.....\xxl111.ilk
........\.....\xxl111.obj
........\.....\xxl111.pdb
........\fort.71
........\shuchu4.dat
........\shuru4.dat
........\xxl111.dsp
........\xxl111.dsw
........\xxl111.f90
........\xxl111.opt
........\xxl111.plg
........\Debug
xxl-xing
