|November 4, 2016, 11:11||
Boundary Condition Values for NASA Rotor 37
Join Date: Jun 2015
Posts: 7Rep Power: 3
Hello guys, I am new to turbomachinery simulation. I am going to perform simulation of Nasa Rotor 37 in Ansys CFX using Turbo Mode. (not stage just rotor).
As per literature i should use Total Pressure inlet and Static Pressure outlet BCs. My questions :
1. What should be the value of Total Inlet Pressure?
2. What should be the value of Reference Pressure ? (1 atm? )
As per the case , we have to change the Static Pressure outlet values from 99215 Pa to 124027 Pa. In order to see the changes in Mass flow rate right?
Kindly guide me and sorry for asking such basic questions.
Thanks in advance
|November 6, 2016, 09:32||
Join Date: Dec 2013
Posts: 23Rep Power: 4
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