solve Euler equations in nozzle with Flux vector splitting method
File list:
Debug
....\BEAM_WARMING_BOUNDARY_SET_1.exe
....\BEAM_WARMING_BOUNDARY_SET_1.pdb
....\DF60.PDB
....\MAIN.obj
BEAM_WARMING_BOUNDARY_SET_1.dsp
BEAM_WARMING_BOUNDARY_SET_1.dsw
BEAM_WARMING_BOUNDARY_SET_1.opt
BEAM_WARMING_BOUNDARY_SET_1.plg
CONVERGENCE_HISTORY.DAT
MAIN.F90
RESULTS.DAT