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ashwininventech
02-02-2011, 05:53 PM
Hello,

I am trying to design cooling system for an electronic heat load of the 2.5 kW in a chamber.

I need to supply air at 17 deg C to maintain the temperature of the air in the chamber at 20 deg C. (As per the specifications)

The chamber is insulated.

In this case how to determine the Air Flow?

Brian_UK
02-02-2011, 06:43 PM
We need a few more details, as usual.

Ambient air temperature
Size of room
Air Change Rate
etc

ashwininventech
03-02-2011, 10:35 AM
Thanks for the reply.

Ambient air temp is 45 deg C (max)
Size of the chamber is 520 mm (width) x 520 mm (Length) x 900 mm (Height)

MilosBog
06-02-2011, 05:00 AM
Q=V*cp*ro*DT/3600
From that
V(air flow)=Q*3600/cp*DT*ro [m3/h]
cp heat capacity of air
ro density
DT-your case 3K
you allready have a Q=2.5kW so just change the units and that is it.
And also you can do it according to the desired air change rate.

dougheret0
08-02-2011, 10:32 PM
KW = air flow * delta T*specific heat of air *density of air*conversion constants
KW = L/s * ˚C * cal/gm˚C *gm/L* kw-hr/cal * s/hr
for air, cal/gm˚C = .25, density gm/L =1.25
s/hr = 3600, kw-hr/cal =1.163*10^-6

so L/s = KW/(˚C * cal/gm˚C *gm/L* kw-hr/cal * s/hr )
= 2.5/(3*.25*1.25*1.163*10^-6*3600)
= 640 L/s

This is the minimum air flow needed to absorb 2.5KW with a temperature rise of 3˚C. Any higher air flow will result in a chamber colder than 20˚C, ultimately approaching the 17˚C supply air temperature.