Description: Face charge calculation of solid rocket motor process of establishing the working pressure
Input for the specific heat ratio, gas gas constant, ignition temperature, propellant density, charge diameter, nozzle throat diameter, charge volume, related to burning rate constant, the ignition pressure output and working hours for the pressure
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File list (Check if you may need any files):
xxl\Debug\DF60.PDB
...\.....\xxl.exe
...\.....\xxl.pdb
...\shuchu1.dat
...\shuru1.dat
...\the establish of Pc.lpk
...\xxl.dsp
...\xxl.dsw
...\xxl.f90
...\xxl.opt
...\xxl.plg
...\Debug
xxl
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