MATHEMATICAL MODELING TO SUPERSONIC OF THE SYMMETRICAL CURRENT OF THE GAS IN NOZZLE WITH PROFILE WITHOUT MOMENT OF THE SHELL
Roblem worded within the framework of classical admissions of the gas track record with initial condition, describing current of the ideal gas in nozzle with profile of without moment of the shell. The considered method of the features, for which is formed разностная scheme and algorithm her numerical realization. Importance of the velocity of the gas is received on output from the nozzle.