: The research paper simulates airflow in a supersonic De Laval nozzle and explores air flow actions isolated from the
local area's nozzle. The pressure levels in the input portion of the nozzle (pressure-inlet condition) and the atmospheric output
parts (pressure-outlet condition) are used to replicate the current model. The fluid divides the motion of a lambda shock, led to a
series of expansion and compression waves; for 1:4 < NPR < 2:4, the estimation shows the probability of an asymmetric flow
structure. Computationally obtained asymmetric flow models are compatible with previous theoretical flow visualization studies.
The nozzle pressure ratio (NPR) is equivalent to balancing the nozzle's inlet air pressure to the ambient pressure. Thus, the value
of the nozzle pressure ratio in the current system is 1.5, and the amount of inlet air pressure and the pressure at the output is
equal to the ambient pressure
