I created a new simulation project called 'Shockwave detection in convergent divergent nozzle':
Project mainly focuses on capturing of shockwave at the outlet of converging diverging nozzle with inlet velocity at 250ms or more . Detection of shock has been main research focus in the field of aerodynamics and numerous effects on the body generating shock . Also data can be used for the study of aeroacoustics for calculation of sound pressure level and sources of acoustics.
More of my public projects can be found here.