Ninja1980
Chemical
- Feb 8, 2007
- 13
I’ve just been asked the question if supersonic flow could occur at any point in the plant we are currently designing. I explained at no point the speed of fluid could exceed Mach 1 (chocked flow) unless flow passes though a convergent-divergent nozzle with sonic flow at the throat and the correct downstream pressure to create supersonic flow in the outlet. This is the same principle used jet engines.
However, this has got me thinking, could supersonic flow could occur though a blowdown valve or PSV? Assuming the back pressure was in the correct limitations, could this act as a De Laval nozzle???
However, this has got me thinking, could supersonic flow could occur though a blowdown valve or PSV? Assuming the back pressure was in the correct limitations, could this act as a De Laval nozzle???