|November 25, 2015, 09:08||
Boundary Conditions Problem
Join Date: Nov 2015
Posts: 1Rep Power: 0
How can I apply 500000 Pascal pressure in nozzle entrance
(the nozzle is in a cabin) ?
Which values must be applied to the following parameters listed below?
1) Operating Pressure = ?
2) Gauge Total Pressure = ?
3) Supersonic/Initial Gauge Pressure = ?
4) Gauge Pressure (into atmosphere from cabin outlet) = ?
I will be glad if you answer to these questions.
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