| Any flow rate with a stated test pressure can be manipulated to calculate the flow at any other test pressure with this formula: CFM2 = CFM1*(P2/P1)^0.5 Where: CFM2 = the flow rate of interest CFM1 = the measured flow rate at X test pressure P2 = the test pressure of interest P1 = the test pressure used to generate CFM1 This works flawlessly up to the point where the velocity in the duct goes supersonic, which will never happen here.
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