
Arturo O. answered 08/07/17
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It looks like an expression to calculate the speed of the air. The total pressure pt is the sum of static pressure ps and dynamic pressure ρv2/2, where v is the speed of the flow and ρ is the air density, which I assume is constant. Assuming no change in pressure due to elevation change,
pt = ps + ρv2/2
v = √[(2/ρ)(pt - ps)] = [√(2/ρ)] √(pt - ps)
Note that √(pt - ps) is the square root of differential pressure. Then √(2/ρ) could be the number in question, in some specific units.
But it could also be a mass flow rate calculation, as in
dm/dt = ρAv,
where A is the cross sectional area of the flow. The speed v would still be [√(2/ρ)] √(pt - ps). Then
dm/dt = ρA [√(2/ρ)] √(pt - ps).
Then the number in question could be ρA [√(2/ρ)] in some specific units.
It could also be a volume flow rate calculation. I would need to know more about what is meant by "air flow." Is it speed of the flow, or mass flow rate of the air, or volume flow rate of the air? I am sure we can figure this out.

Arturo O.
08/07/17