Fwann15
Student
- Mar 24, 2021
- 11
I'm designing a turbine test rig, and for the air supply system, I'm thinking to have a compressor connected to an air receiver, then to a back pressure regulator, and finally to a converging nozzle connected to the turbine. There are some known variables, the turbine nozzle inlet diameter is 77mm, the mass flow rate at the inlet is suggested to be 0.7kg/s, and the compressed air should be around 7.5 bar. I'm struggling to find any air tanks/receivers that have an exit area of 77mm or higher, and I'm not even sure if this design is the best for my test rig. Will really appreciate it if anyone could suggest a better air supply system and where I can find the relevant components. Thanks!