I was working on a project the other day with a process engineer when he told me that the program he was using to evaulate relief valve scenarios gave him a Mach number of 0.9 for one of our relief valves. We both thought this was incorrect since the vessel is at 70 psi pressure and ambient temperature. The orifice is an "M" sized orifice (I think this is about a 1" diameter opening).
It did make me wander what size orifice we would need to result in a Mach 1 speed through the orifice. I did similar problems in college so I thought I would treat it as a converging nozzle with a choked area. I quickly found out that I didn't remember as much about the topic as I thought I did so I thought I would defer to CR4.
Do I have enough information here to find the area needed to choke the flow? Assume we use air for the fluid.