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Old   November 25, 2015, 09:08
Default Boundary Conditions Problem
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sivil aviation
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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.
Best Wishes.
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