Cooling of Moist Air
Outdoor air at sea level enters an air conditioner’s cooling coil at 2000 ft³/min (944 L/s). The inlet dry-bulb condition is 100°F (38°C) and the wetbulb condition is 75°F (24°C). The air is cooled to a dry-bulb temperature of 55°F (13°C) and 90% RH. Assume that the liquid water leaves the coil at 50°F.
(a) Find the total heat transfer rate as well as the sensible and latent cooling loads on the coil.
(b) Determine the sensible heat factor, apparatus dew point, and the bypass factor of the cooling coil.
Given: \dot{V}_{1} = 2000 cfm, T_{db1} = 100°F, T_{wb1} = 75°F, T_{db2} = 55°F, \phi_{2} = 0.9, and T_{cc,liq} = 50°F.
Figure: See Figure 13.16.
Find: \dot{Q}_{tot c}, \dot{Q}_{sen},\dot{Q}_{lat}, SHF_{cc}, ADP, BP_{cc}.
Lookup values: The enthalpy of liquid water at 50°F is 18.06 Btu/lb_{w} from Table A3. From the sea-level psychrometric chart, we determine the following inlet and outlet values in IP units:
State | W, lb_{w}/lb_{a} | h, Btu/lb_{a} | v, ft^{3}/lb_{a} |
1 | 0.013 | 38.4 | 14.4 |
2 | 0.0083 | 22.2 | – |
TABLE A.3 (IP Units) Properties of Saturated Steam | ||||||||||||
Pressure (psia) | Saturation Temp. (°F) | Specific Volume (ft³/lb_{m}) |
Internal Energy (Btu/lb_{m}) | Enthalpy (Btu/lb_{m}) | Entropy (Btu/(lb_{m} · °R)) | |||||||
Sat. Liquid | Sat. Vapor | Sat. Liquid | Evap. | Sat. Vapor | Sat. Liquid | Evap. | Sat. Vapor | Sat. Liquid | Evap. | Sat. Vapor | ||
p | Tsat | vf | vg | uf | ufg | ug | hf | hfg | hg | sf | sfg | sg |
0.08866 | 32.02 | 0.016022 | 3302 | 0.00 | 1021.2 | 1021.2 | 0.01 | 1075.4 | 1075.4 | 0.00000 | 2.1869 | 2.1869 |
0.09992 | 35.00 | 0.016021 | 2948 | 2.99 | 1019.2 | 1022.2 | 3.00 | 1073.7 | 1076.7 | 0.00607 | 2.1704 | 2.1764 |
0.12166 | 40.00 | 0.016020 | 2445 | 8.02 | 1015.8 | 1023.9 | 8.02 | 1070.9 | 1078.9 | 0.01617 | 2.1430 | 2.1592 |
0.14748 | 45.00 | 0.016021 | 2037 | 13.04 | 1012.5 | 1025.5 | 13.04 | 1068.1 | 1081.1 | 0.02618 | 2.1162 | 2.1423 |
0.17803 | 50.00 | 0.016024 | 1704.2 | 18.06 | 1009.1 | 1027.2 | 18.06 | 1065.2 | 1083.3 | 0.03607 | 2.0899 | 2.1259 |
0.2563 | 60.00 | 0.016035 | 1206.9 | 28.08 | 1002.4 | 1030.4 | 28.08 | 1059.6 | 1087.7 | 0.05555 | 2.0388 | 2.0943 |
0.3632 | 70.00 | 0.016051 | 867.7 | 38.09 | 995.6 | 1033.7 | 38.09 | 1054.0 | 1092.0 | 0.07463 | 1.9896 | 2.0642 |
0.5073 | 80.00 | 0.016073 | 632.8 | 48.08 | 988.9 | 1037.0 | 48.09 | 1048.3 | 1096.4 | 0.09332 | 1.9423 | 2.0356 |
0.6988 | 90.00 | 0.016099 | 467.7 | 58.07 | 982.2 | 1040.2 | 58.07 | 1042.7 | 1100.7 | 0.11165 | 1.8966 | 2.0083 |
0.9503 | 100.00 | 0.016130 | 350.0 | 68.04 | 975.4 | 1043.5 | 68.05 | 1037.0 | 1105.0 | 0.12963 | 1.8526 | 1.9822 |
1 | 101.70 | 0.016136 | 333.6 | 69.74 | 974.3 | 1044.0 | 69.74 | 1036.0 | 1105.8 | 0.13266 | 1.8453 | 1.9779 |
2 | 126.04 | 0.016230 | 173.75 | 94.02 | 957.8 | 1051.8 | 94.02 | 1022.1 | 1116.1 | 0.17499 | 1.7448 | 1.9198 |
3 | 141.43 | 0.016300 | 118.72 | 109.38 | 947.2 | 1056.6 | 109.39 | 1013.1 | 1122.5 | 0.20089 | 1.6852 | 1.8861 |
4 | 152.93 | 0.016358 | 90.64 | 120.88 | 939.3 | 1060.2 | 120.89 | 1006.4 | 1127.3 | 0.21983 | 1.6426 | 1.8624 |
5 | 162.21 | 0.016407 | 73.53 | 130.15 | 932.9 | 1063.0 | 130.17 | 1000.9 | 1131.0 | 0.23486 | 1.6093 | 1.8441 |
6 | 170.03 | 0.016451 | 61.98 | 137.98 | 927.4 | 1065.4 | 138.00 | 996.2 | 1134.2 | 0.24736 | 1.5819 | 1.8292 |
8 | 192.84 | 0.016526 | 47.35 | 150.81 | 918.4 | 1069.2 | 150.84 | 988.4 | 1139.3 | 0.26754 | 1.5383 | 1.8058 |
10 | 193.19 | 0.016590 | 38.42 | 161.20 | 911.0 | 1072.2 | 161.23 | 982.1 | 1143.3 | 0.28358 | 1.5041 | 1.7877 |
14.696 | 211.99 | 0.016715 | 26.80 | 180.10 | 897.5 | 1077.6 | 180.15 | 970.4 | 1150.5 | 0.31212 | 1.4446 | 1.7567 |
15 | 213.03 | 0.016723 | 26.29 | 181.14 | 896.8 | 1077.9 | 181.19 | 969.7 | 1150.9 | 0.31367 | 1.4414 | 1.7551 |
20 | 227.96 | 0.016830 | 20.09 | 196.19 | 885.8 | 1082.0 | 196.26 | 960.1 | 1156.4 | 0.33580 | 1.3962 | 1.7320 |
25 | 240.08 | 0.016922 | 16.306 | 208.44 | 876.9 | 1085.3 | 208.52 | 952.2 | 1160.7 | 0.35345 | 1.3607 | 1.7142 |
30 | 250.34 | 0.017004 | 13.748 | 218.84 | 869.2 | 1088.0 | 218.93 | 945.4 | 1164.3 | 0.36821 | 1.3314 | 1.6996 |
35 | 259.30 | 0.017073 | 11.900 | 227.93 | 862.4 | 1090.3 | 228.04 | 939.3 | 1167.4 | 0.38093 | 1.3064 | 1.6873 |
40 | 267.26 | 0.017146 | 10.501 | 236.03 | 856.2 | 1092.3 | 236.16 | 933.8 | 1170.0 | 0.39214 | 1.2845 | 1.6767 |
45 | 274.46 | 0.017209 | 9.403 | 243.37 | 850.7 | 1094.0 | 243.51 | 928.8 | 1172.3 | 0.40218 | 1.2651 | 1.6673 |
50 | 281.03 | 0.017269 | 8.518 | 250.08 | 845.5 | 1095.6 | 250.24 | 924.2 | 1174.4 | 0.41129 | 1.2476 | 1.6589 |
55 | 287.10 | 0.017325 | 7.789 | 256.28 | 840.8 | 1097.0 | 256.46 | 919.9 | 1176.3 | 0.41963 | 1.2317 | 1.6513 |
60 | 292.73 | 0.017378 | 7.177 | 262.06 | 836.3 | 1098.3 | 262.25 | 915.8 | 1178.0 | 0.42733 | 1.2170 | 1.6444 |
65 | 298.00 | 0.017429 | 6.657 | 267.46 | 832.1 | 1099.5 | 267.67 | 911.9 | 1179.6 | 0.43450 | 1.2035 | 1.6380 |
70 | 302.96 | 0.017478 | 6.209 | 272.56 | 828.1 | 1100.6 | 272.79 | 908.3 | 1181.0 | 0.44120 | 1.1909 | 1.6321 |
75 | 307.63 | 0.017524 | 5.818 | 277.37 | 824.3 | 1101.6 | 277.61 | 904.8 | 1182.4 | 0.44749 | 1.1790 | 1.6265 |
80 | 312.07 | 0.017570 | 5.474 | 281.95 | 820.6 | 1102.6 | 282.21 | 901.4 | 1183.6 | 0.45344 | 1.1679 | 1.6214 |
85 | 316.29 | 0.017613 | 5.17 | 286.3 | 817.1 | 1103.5 | 286.58 | 898.2 | 1184.8 | 0.45907 | 1.1574 | 1.6165 |
90 | 320.31 | 0.017655 | 4.898 | 290.46 | 813.8 | 1104.3 | 290.76 | 895.1 | 1185.9 | 0.46442 | 1.1475 | 1.6119 |
95 | 324.16 | 0.017696 | 4.654 | 294.45 | 810.6 | 1105.0 | 294.76 | 892.1 | 1186.9 | 0.46952 | 1.1380 | 1.6076 |
100 | 327.86 | 0.017736 | 4.434 | 298.28 | 807.5 | 1105.8 | 298.61 | 889.2 | 1187.8 | 0.47439 | 1.1290 | 1.6034 |
110 | 334.82 | 0.017813 | 4.051 | 305.52 | 801.6 | 1107.1 | 305.88 | 883.7 | 1189.6 | 0.48355 | 1.1122 | 1.5957 |
120 | 341.30 | 0.017886 | 3.73 | 312.27 | 796 | 1108.3 | 312.67 | 878.5 | 1191.1 | 0.49201 | 1.0966 | 1.5886 |
130 | 347.37 | 0.017957 | 3.457 | 318.61 | 790.7 | 1109.4 | 319.04 | 873.5 | 1192.5 | 0.49989 | 1.0822 | 1.5821 |
140 | 353.08 | 0.018024 | 3.221 | 324.58 | 785.7 | 1110.3 | 325.05 | 868.7 | 1193.8 | 0.50727 | 1.0688 | 1.5761 |
150 | 358.48 | 0.018089 | 3.016 | 330.24 | 781 | 1111.2 | 330.75 | 864.2 | 1194.9 | 0.51422 | 1.0562 | 1.5704 |
0.6113 | 0.01 | 0.001 | 206.14 | 0 | 2375.3 | 2375.3 | 0.01 | 2501.3 | 2501.4 | 0 | 9.1562 | 9.1562 |
1.0 | 6.98 | 0.001 | 129.21 | 29.30 | 2355.7 | 2385.0 | 29.30 | 2484.9 | 2514.2 | 0.1059 | 8.8697 | 8.9756 |
1.5 | 13.03 | 0.001001 | 87.98 | 54.71 | 2338.6 | 2393.3 | 54.71 | 2470.6 | 2525.3 | 0.1957 | 8.6322 | 8.8279 |
2.0 | 17.50 | 0.001001 | 67.00 | 73.48 | 2326.0 | 2399.5 | 73.48 | 2460.0 | 2533.5 | 0.2607 | 8.4629 | 8.7237 |
2.5 | 21.08 | 0.001002 | 54.25 | 88.48 | 2315.9 | 2404.4 | 88.49 | 2451.6 | 2540.4 | 0.3120 | 8.3311 | 8.6432 |
3.0 | 24.08 | 0.001003 | 45.67 | 101.04 | 2307.5 | 2408.5 | 101.05 | 2444.5 | 2545.5 | 0.3545 | 8.2231 | 8.5776 |
4.0 | 28.96 | 0.001004 | 34.80 | 121.45 | 2293.7 | 2415.2 | 121.46 | 2432.9 | 2554.4 | 0.4226 | 8.0520 | 8.4746 |
5.0 | 32.88 | 0.001005 | 28.19 | 137.81 | 2282.7 | 2420.5 | 137.82 | 2423.7 | 2561.5 | 0.4764 | 7.9187 | 8.3951 |
7.5 | 40.29 | 0.001008 | 19.24 | 168.78 | 2261.7 | 2430.5 | 168.79 | 2406.0 | 2574.8 | 0.5764 | 7.6750 | 8.2515 |
10 | 45.81 | 0.001010 | 14.67 | 191.82 | 2246.1 | 2437.9 | 191.83 | 2392.8 | 2584.7 | 0.6493 | 7.5009 | 8.1502 |
15 | 53.97 | 0.001014 | 10.02 | 225.92 | 2222.8 | 2448.7 | 225.94 | 2373.1 | 2599.1 | 0.7549 | 7.2536 | 8.0085 |
20 | 60.06 | 0.001017 | 7.649 | 251.38 | 2205.4 | 2456.7 | 251.40 | 2358.3 | 2609.7 | 0.8320 | 7.0766 | 7.9085 |
25 | 64.97 | 0.001020 | 6.204 | 271.90 | 2191.2 | 2463.1 | 271.93 | 2346.3 | 2618.2 | 0.8931 | 6.9383 | 7.8314 |
30 | 69.10 | 0.001022 | 5.229 | 289.20 | 2179.2 | 2468.4 | 289.23 | 2336.1 | 2625.3 | 0.9439 | 6.8247 | 7.7686 |
40 | 75.87 | 0.001027 | 3.993 | 317.53 | 2159.5 | 2477.0 | 317.58 | 2319.2 | 2636.8 | 1.0259 | 6.6441 | 7.6700 |
50 | 81.33 | 0.001030 | 3.240 | 340.44 | 2143.4 | 2483.9 | 340.49 | 2305.4 | 2645.9 | 1.0910 | 6.5029 | 7.5939 |
75 | 91.78 | 0.001037 | 2.217 | 384.31 | 2112.4 | 2496.7 | 384.39 | 2278.6 | 2663.0 | 1.2130 | 6.2434 | 7.4564 |
100 | 99.63 | 0.001043 | 1.6940 | 417.36 | 2088.7 | 2506.1 | 417.46 | 2258.0 | 2675.5 | 1.3026 | 6.0568 | 7.3594 |
125 | 105.99 | 0.001048 | 1.3749 | 444.19 | 2069.3 | 2513.5 | 444.32 | 2241.0 | 2685.4 | 1.3740 | 5.9104 | 7.2844 |
150 | 111.37 | 0.001053 | 1.1593 | 466.94 | 2052.7 | 2519.7 | 467.11 | 2226.5 | 2693.6 | 1.4336 | 5.7897 | 7.2233 |
175 | 116.06 | 0.001057 | 1.0036 | 486.8 | 2038.1 | 2524.9 | 486.99 | 2213.6 | 2700.6 | 1.4849 | 5.6868 | 7.1717 |
200 | 120.23 | 0.001061 | 0.8857 | 504.49 | 2025.0 | 2529.5 | 504.70 | 2201.9 | 2706.7 | 1.5301 | 5.5970 | 7.1271 |
225 | 124 | 0.001064 | 0.7933 | 520.47 | 2013.1 | 2533.6 | 520.72 | 2191.3 | 2712.1 | 1.5706 | 5.5173 | 7.0878 |
250 | 127.44 | 0.001067 | 0.7187 | 535.10 | 2002.1 | 2537.2 | 535.37 | 2181.5 | 2716.9 | 1.6072 | 5.4455 | 7.0527 |
275 | 130.6 | 0.001070 | 0.6573 | 548.59 | 1991.9 | 2540.5 | 548.89 | 2172.4 | 2721.3 | 1.6408 | 5.3801 | 7.0209 |
300 | 133.55 | 0.001073 | 0.6058 | 561.15 | 1982.4 | 2543.6 | 561.47 | 2163.8 | 2725.3 | 1.6718 | 5.3201 | 6.9919 |
325 | 136.3 | 0.001076 | 0.5620 | 572.90 | 1973.5 | 2546.4 | 573.25 | 2155.8 | 2729.0 | 1.7006 | 5.2646 | 6.9652 |
350 | 138.88 | 0.001079 | 0.5243 | 583.95 | 1965.0 | 2548.9 | 584.33 | 2148.1 | 2732.4 | 1.7275 | 5.2130 | 6.9405 |
375 | 141.32 | 0.001081 | 0.4914 | 594.40 | 1956.9 | 2551.3 | 594.81 | 2140.8 | 2735.6 | 1.7528 | 5.1647 | 6.9175 |
400 | 143.63 | 0.001084 | 0.4625 | 604.31 | 1949.3 | 2553.6 | 604.74 | 2133.8 | 2738.6 | 1.7766 | 5.1193 | 6.8959 |
450 | 147.93 | 0.001088 | 0.4140 | 622.77 | 1934.9 | 2557.6 | 623.25 | 2120.7 | 2743.9 | 1.8207 | 5.0359 | 6.8565 |
500 | 151.86 | 0.001093 | 0.3749 | 639.68 | 1921.6 | 2561.2 | 640.23 | 2108.5 | 2748.7 | 1.8607 | 4.9606 | 6.8213 |
550 | 155.48 | 0.001097 | 0.3427 | 655.32 | 1909.2 | 2564.5 | 655.93 | 2097.0 | 2753.0 | 1.8973 | 4.8920 | 6.7893 |
600 | 158.85 | 0.001101 | 0.3157 | 669.90 | 1897.5 | 2567.4 | 670.56 | 2086.3 | 2756.8 | 1.9312 | 4.8288 | 6.7600 |
650 | 162.01 | 0.001104 | 0.2927 | 683.56 | 1886.5 | 2570.1 | 684.28 | 2076.0 | 2760.3 | 1.9627 | 4.7703 | 6.7331 |
700 | 164.97 | 0.001108 | 0.2729 | 696.44 | 1876.1 | 2572.5 | 697.22 | 2066.3 | 2763.5 | 1.9922 | 4.7158 | 6.7080 |
750 | 167.78 | 0.001112 | 0.2556 | 708.64 | 1866.1 | 2574.7 | 709.47 | 2057.0 | 2766.4 | 2.0200 | 4.6647 | 6.6847 |
800 | 170.43 | 0.001115 | 0.2404 | 720.22 | 1856.6 | 2576.8 | 721.11 | 2048.0 | 2769.1 | 2.0462 | 4.6166 | 6.6628 |
850 | 172.96 | 0.001118 | 0.2270 | 731.27 | 1847.4 | 2578.7 | 732.22 | 2039.4 | 2771.6 | 2.0710 | 4.5711 | 6.6421 |
900 | 175.38 | 0.001121 | 0.2150 | 741.83 | 1838.6 | 2580.5 | 742.83 | 2031.1 | 2773.9 | 2.0946 | 4.5280 | 6.6226 |
950 | 177.69 | 0.001124 | 0.2042 | 751.95 | 1830.2 | 2582.1 | 753.02 | 2023.1 | 2776.1 | 2.1172 | 4.4869 | 6.6041 |
1000 | 179.91 | 0.001127 | 0.19444 | 761.68 | 1822.0 | 2583.6 | 762.81 | 2015.3 | 2778.1 | 2.1387 | 4.4478 | 6.5865 |
1100 | 184.09 | 0.001133 | 0.17753 | 780.09 | 1806.3 | 2586.4 | 781.34 | 2000.4 | 2781.7 | 2.1792 | 4.3744 | 6.5536 |
1200 | 187.99 | 0.001139 | 0.16333 | 797.29 | 1791.5 | 2588.8 | 798.65 | 1986.2 | 2784.8 | 2.2166 | 4.3067 | 6.5233 |
1300 | 191.64 | 0.001144 | 0.15125 | 813.44 | 1777.5 | 2591.0 | 814.93 | 1972.7 | 2787.6 | 2.2515 | 4.2438 | 6.4953 |
Source: Courtesy of ASHRAE, Handbook of Fundamentals, American Society of Heating, Refrigerating and Air-Conditioning Engineers, Atlanta, GA, 1997. With permission. |
(a) First, we will find the mass flow rate:
\dot{m}_{a} = \frac{2000 ft^{3}/min \times 60 min/h}{14.4 ft^{3}/lb_{a}} = 8333 lb_{a}/hThen, using Equation 13.42, the heat rate can be found since all values on the right-hand side are known:
\dot{Q}_{tot,c} = \dot{m}_{a} [(h_{1} – h_{2}) – h_{liq} (W_{1} – W_{2}) ] (13.42)
\dot{Q}_{tot} = \dot{m}_{a} [(h_{1} – h_{2}) – h_{liq} (W_{1} – W_{2}) ]= 8,333 lb_{a}/h \times [(38.4 – 22.2) Btu/lb_{a}
– 18.06 Btu/lb_{w} \times (0.013 – 0.0083) lb_{w}/lb_{a} ]
= (134,995 – 707.3) Btu/h = 134.3 kBtu/h(39.3 kW)
= 11.2 tons of cooling
In order to determine the contributions of the sensible and latent coil loads, we locate point “a” as the intersection on the psychrometric chart of a horizontal line drawn from point 2 and the vertical line drawn from point 1. The enthalpy is found to be h_{a} = 33.8 Btu/lb_{a}.
From Equation 13.43,
\dot{Q}_{sen} = \dot{m}_{a}(h_{a} – h_{2}) (13.43)
\dot{Q}_{sen} = 8,333 lb_{a}/h \times (33.8 – 22.2) Btu/lb_{a}= 96,663 Btu/h = 8.06 tons
and from Equation 13.44,
\dot{Q}_{lat} = \dot{m}_{a} (h_{1} – h_{a}) (13.44)
\dot{Q}_{lat} = 8,333 lb_{a}/h \times (38.4 – 33.8) Btu/lb_{a}= 38,332 Btu/h = 3.19 tons
Finally, the total cooling load on the coil is
\dot{Q}_{tot,c} = \dot{Q}_{sen} + \dot{Q}_{lat} = 134,995 Btu/h = 11.25 tonsIt is instructive to compare these values with those from the simplied approach often adopted for hand calculations. The average specic heat of the air water mixture is (Equation 13.25)
c_{p,m} = c_{p,a} + W \cdot c_{p,vap} = 0.24 + \frac{0.444 \times (0.013 + 0.0083)}{2}= 0.245 Btu/(lb_{a} \cdot °F)
Then, from Equation 13.45
\dot{Q}_{sen} = \dot{m}_{a} c_{p,m} (T_{db1} – T_{db2}) (13.45)
\dot{Q}_{sen} = 8,333 lb_{a}/h \times 0.245 Btu/lb_{a} \cdot °F\times (100 – 55) Btu/lb_{a}
= 91,871 Btu/h = 7.66 tons
And from Equation 13.46,
\dot{Q}_{lat} = \dot{m}_{a} h_{vap} (W_{1} – W_{2}) (13.46)
\dot{Q}_{lat} = 8,333 lb_{a}/h \times 1075 Btu/lb_{liq}\times (0.013 – 0.0083) lb_{w}/lb_{a}
= 42,102 Btu/h = 3.51 tons
Finally,
\dot{Q}_{tot,c} = 91,871 + 42,102 = 133,973 Btu/h = 11.16 tonsNote that the differences in the sensible, latent, and total loads by both methods are −5%, +10%, and less than 1%, respectively.
(b) The cooling coil sensible heat factor is
We draw a straight line between points 1 and 2 extending till the saturated line (not shown in Figure 13.16). The corresponding dry-bulb temperature T_{3} is the ADP, and this is read off as ADP = T_{db3} = 50°F.
Finally, from Equation 13.48, we find
= \frac{Segment 2 – 3}{Segment 1 – 3} = \frac{T_{db2} – T_{db3}}{T_{db1} – T_{db3}} (13.48)
BP_{cc} = \frac{T_{db2} – T_{db3}}{T_{db1} – T_{db3}} = \frac{55 – 50}{100 – 50} = 0.1Comments
This cooling effect must be provided by the chiller. Note that the amount of energy leaving the coil in the form of liquid condensate for this problem (707 Btu/h as determined earlier) is very small, about 0.5% of the total coil load.