CPU Flow Calculator


This calculator allows you to input the Static Pressure, Differential Pressure, and Temperature from the gauges on a Tronair Cabin Pressurization Unit and the resultant output will be the flow and mass flows. This is provided as an alternative method to using the curves provided in the operation and technical manual.

MODELS: 15-7600-1000, 15-7602-1000, 15-7603-1000, 15*7603-1000 (* = letters A through K)
Aircraft Manufacturer:
Aircraft Model:
Aircraft Regsistration #:
 
System Pressure from Pressure Gauge (NOT cabin pressure):   psi (0-15 psi)  
Differential Pressure from Magnahelic or Capsuhelic Pressure Gauge:   inWC (0-20 inches of water column)  
Temperature from Temperature Gauge:   F (50-300 degrees F)  


 
Results
Flow in SCFM:
Mass Flow in lb/hr:
Mass Flow in lb/min:
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