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Handbook of air conditioning and refrigeration / Shan K

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17.54 CHAPTER SEVENTEEN<br />

Static Regain Method<br />

according to the requirement to float the particles, either by calculation or by experience. On the basis<br />

<strong>of</strong> the determined <strong>air</strong> velocity, the cross-sectional area <strong>and</strong>, therefore, the dimension <strong>of</strong> the duct<br />

can be estimated <strong>and</strong> then rounded to a st<strong>and</strong>ard size. The total pressure loss <strong>of</strong> the duct system �p t,<br />

in in. WC (Pa), along the critical path can be calculated as<br />

�pt � K�<br />

2g �� c<br />

f1L1 D1 � � � ��� f nL n<br />

D n<br />

� C 1� v 1 2 �� f 2L 2<br />

D 2<br />

� C n� v n 2�<br />

� C 2� v 2 2<br />

(17.76)<br />

where v 1, v 2,...,v n � mean <strong>air</strong> velocity at duct sections 1, 2, ...,n, respectively, fpm (m/s)<br />

C 1, C 2,...,C n � local loss coefficients at duct sections 1, 2, ...,n, respectively<br />

K � 5.35 � 10 �5 for I-P unit (1 for SI unit)<br />

This method sizes the <strong>air</strong> duct so that the increase <strong>of</strong> static pressure (static regain) due to the reduction<br />

<strong>of</strong> <strong>air</strong> velocity in the supply main duct after each branch take<strong>of</strong>f nearly <strong>of</strong>fsets the pressure loss<br />

<strong>of</strong> the succeeding duct section along the main duct. As a consequence, the static pressure at the<br />

common end <strong>of</strong> the diverging tee or wye <strong>of</strong> the sized duct section remains approximately the same<br />

as that <strong>of</strong> the preceding section.<br />

A rectangular duct section 1-2 between the cross-sectional planes 1 <strong>and</strong> 2 is illustrated in<br />

Fig. 17.22. The size <strong>of</strong> this duct section is to be determined. Let v 1 <strong>and</strong> v 2 be the mean velocities at<br />

FIGURE 17.22 Pressure characteristics <strong>of</strong> a main duct section.

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