130 CHEMICAL ENGINEERING VOLUME 1 SOLUTIONS
Film coefficients
Inside:
hidi/kD 0. 023
dG^0 /^0.^8
Cp/k^0.^4 (equation 9.61)
diD12 mm or 1. 2 ð 10 ^2 m.
The mean air temperatureD 0. 5
366 C 283 D325 K andkD 0 .029 W/m K.
Cross-sectional area of one tubeD
$/ 4
1. 2 ð 10 ^22 D 1. 131 ð 10 ^4 m^2
Area for flowD
20 ð 201. 131 ð 10 ^4 D 4. 52 ð 10 ^2 m^2.
Thus, mass velocityGD 0. 9 /
4. 52 ð 10 ^2 D 19 .9 kg/m^2 s.
At 325 K,D 0 .0198 mN s/m^2 or 1. 98 ð 10 ^5 Ns/m^2
CpD
1. 0 ð 103 J/kg K
Thus:
hið 1. 2 ð 10 ^2 /
2. 9 ð 10 ^2 D 0. 023
- 2 ð 10 ^2 ð 19. 9 / 1. 98 ð 10 ^50.^8
ð
1. 0 ð 103 ð 1. 98 ð 10 ^5 / 0. 0290.^4
0. 4138 hiD 0. 023
1. 206 ð 1040.^8
0. 6830.^4 and hiD 87 .85 W/m^2 K
Outside:
hodo/kD 0. 33 Ch
doG^0 /^0 max.^6
Cp/k^0.^3 (equation 9.90)
doD 12 .0mm or 1. 2 ð 10 ^2 m
G^0 D10 kg/m^2 s for free flow
G^0 maxDYG^0 /
Ydo
whereY, the distance between tube centresD 2 doD 2. 4 ð 10 ^2 m.
∴ G^0 maxD
2. 4 ð 10 ^2 ð 10. 0 /
2. 4 ð 10 ^2 1. 2 ð 10 ^2 D20 kg/m^2 s
At a mean flue gas temperature of 0. 5
700 C 366 D533 K,
D 0 .0286 mN s/m^2 or 2. 86 ð 10 ^5 Ns/m^2 , kD 0 .045 W/m K and CpD
- 0 ð
103 J/kg K
∴ RemaxD
- 2 ð 10 ^2 ð 20. 0 /
- 86 ð 10 ^5 D 8. 39 ð 103
From Table 9.3, whenRemaxD 8. 39 ð 103 ,XD 2 do,andYD 2 do,ChD 0 .95.
Thus:
hoð 1. 2 ð 10 ^2 /
4. 5 ð 10 ^2 D
0. 33 ð 0. 95
8. 39 ð 1030.^6
ð
1. 0 ð 103 ð 2. 86 ð 10 ^5 / 0. 0450.^3
or: 0. 267 hoD 0. 314
8. 39 ð 1030.^6
0. 8360.^3 and hoD232 W/m^2 K
Overall:
Ignoring wall and scale resistances, then:
1 /UD 1 /hoC 1 /hiD
0. 0114 C 0. 0043 D 0. 0157
and: UD 63 .7W/m^2 K