The effect of opening angle on shock patterns in supersonic jets

Movies in the form of animated gifs.

Corresponding to figures, table and notation of paper submitted to MNRAS with the same title.

Movies of jets exiting a circular nozzle with a

Half-opening angle A in degrees,

Mach number M,  

overpressure relative to ambient K and

density D  relative to the ambient medium. 

All simulations run to 200 time units.

Adiabatic gas with specific heat ratio of 5/3. 

These are all pressure movies with the ambient pressure set to 0.6., ambient sound speed and density both unity.