Boundary Conditions Problem -- CFD Online Discussion Forums

November 25, 2015, 08:08	Boundary Conditions Problem	#1
airframe New Member sivil aviation Join Date: Nov 2015 Posts: 1 Rep 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. Best Wishes.

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