Two nested spherical tanks with the internal and outer diameters of the 100 cm by 104 cm and 114 cm by 118 cm is used to store hot water at 100°C. Both tanks are made of boron fiber epoxy with different composite compositions. The thermal conductivity of the inner tank is 1.5 W/m K while the outer tank has a thermal conductivity of 0.5 W/m K. The gap between the tanks is filled with air (use properties of air at 50°C). The tank is located in an open environment at 0'C. The outer surface of the tank is white painted and heat transfer between the outer surface of the tank and the surrounding is by natural covection and radiation. The convection heat transfer coefficient at the inner and the outer surface of the pipe is h= 20 W/m' K and h,= 10 W/m K. Determine ; a. the rate of heat loss from the tank b. the inside, outside and intermediate surface temperatures. Hint: Take the outer surface temperature as 3°C for radiation calculations.
Two nested spherical tanks with the internal and outer diameters of the 100 cm by 104 cm and 114 cm by 118 cm is used to store hot water at 100°C. Both tanks are made of boron fiber epoxy with different composite compositions. The thermal conductivity of the inner tank is 1.5 W/m K while the outer tank has a thermal conductivity of 0.5 W/m K. The gap between the tanks is filled with air (use properties of air at 50°C). The tank is located in an open environment at 0'C. The outer surface of the tank is white painted and heat transfer between the outer surface of the tank and the surrounding is by natural covection and radiation. The convection heat transfer coefficient at the inner and the outer surface of the pipe is h= 20 W/m' K and h,= 10 W/m K. Determine ; a. the rate of heat loss from the tank b. the inside, outside and intermediate surface temperatures. Hint: Take the outer surface temperature as 3°C for radiation calculations.
Principles of Heat Transfer (Activate Learning with these NEW titles from Engineering!)
8th Edition
ISBN:9781305387102
Author:Kreith, Frank; Manglik, Raj M.
Publisher:Kreith, Frank; Manglik, Raj M.
Chapter9: Heat Transfer With Phase Change
Section: Chapter Questions
Problem 9.37P
Related questions
Question
![Two nested spherical tanks with the internal and outer
diameters of the 100 cm by 104 cm and 114 cm by 118 cm is
used to store hot water at 100 C. Both tanks are made of boron
fiber epoxy with different composite compositions. The
thermal conductivity of the inner tank is 1.5 W/m K while the
outer tank has a thermal conductivity of 0.5 W/m K. The gap
between the tanks is filled with air (use properties of air at
50°C). The tank is located in an open environment at 0'C. The
outer surface of the tank is white painted and heat transfer
between the outer surface of the tank and the surrounding is
by natural covection and radiation. The convection heat
transfer coefficient at the inner and the outer surface of the
pipe is h 20 W/m' K and h 10 W/m K. Determine;
a. the rate of heat loss from the tank
b. the inside, outside and intermediate surface temperatures.
Hint: Take the outer surface temperature as 3°C for radiation
calculations.](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F4447d9cc-345f-4198-8b5a-0a8b631bec55%2F0dd2ecbf-3091-40b4-9758-07608660fba5%2Fbdnkq7f_processed.jpeg&w=3840&q=75)
Transcribed Image Text:Two nested spherical tanks with the internal and outer
diameters of the 100 cm by 104 cm and 114 cm by 118 cm is
used to store hot water at 100 C. Both tanks are made of boron
fiber epoxy with different composite compositions. The
thermal conductivity of the inner tank is 1.5 W/m K while the
outer tank has a thermal conductivity of 0.5 W/m K. The gap
between the tanks is filled with air (use properties of air at
50°C). The tank is located in an open environment at 0'C. The
outer surface of the tank is white painted and heat transfer
between the outer surface of the tank and the surrounding is
by natural covection and radiation. The convection heat
transfer coefficient at the inner and the outer surface of the
pipe is h 20 W/m' K and h 10 W/m K. Determine;
a. the rate of heat loss from the tank
b. the inside, outside and intermediate surface temperatures.
Hint: Take the outer surface temperature as 3°C for radiation
calculations.
![TABLE A-15
Properties of air at 1 atm pressure
Dynamic
Viscosity
µ, kg/m-s
Kinematic
Prandtl
Specific
Heat
Thermal
Thermal
Temp.
T, °C
Conductivity
k, W/m-K
Density
Diffusivity
Viscosity
v, m?/s
Number
P, kg/m³
Cp, J/kg-K
a, m?/s
Pr
-150
-100
8.636 x 10-6
1.189 x 10-5
2.866
983
0.01171
4.158 x 10-6
3.013 x 10-6
0.7246
8.036 x 10-6
1.252 x 10-5
1.356 x 10-5
1.465 x 10-5
1.578 x 10-5
1.696 x 10-5
2.038
966
0.01582
5.837 x 10-6
0.7263
0.01979
0.02057
-50
1.582
999
1.474 x 10-5
9.319 x 10-6
0.7440
1.527 x 10-5
1.579 x 10-5
1.630 x 10-5
1.680 x 10-5
1.729 x 10-5
1.754 x 10-5
1.778 x 10-5
1.802 x 10-5
1.825 x 10-5
1.849 x 10-5
1.872 x 10-5
-40
-30
1.514
1.451
1002
1004
1.008 x 10-5
1.087 x 10-5
0.7436
0.7425
0.7408
0.02134
0.02211
0.02288
-20
1.394
1005
1.169 x 10-5
-10
1.341
1006
1.252 x 10-5
0.7387
1.292
1006
0.02364
1.818 x 10-5
1.338 x 10-5
0.7362
1.880 x 10-5
1.944 x 10-5
2.009 x 10-5
2.074 x 10-5
2.141 x 10-5
2.208 x 10-5
1.269
1006
0.02401
1.382 x 10-5
0.7350
1.246
1.225
10
1006
0.02439
1.426 x 10-5
0.7336
15
1007
0.02476
1.470 x 10-5
0.7323
1007
1007
1007
1.516 x 10-5
1.562 x 10-5
1.608 x 10-5
1.655 x 10-5
20
1.204
0.02514
0.7309
25
1.184
0.02551
0.7296
30
1.164
0.02588
0.7282
35
1.145
1007
0.02625
2.277 x 10-5
1.895 x 10-5
0.7268
2.346 x 10-5
2.416 x 10-5
2.487 x 10-5
2.632 x 10-5
2.780 x 10-5
2.931 x 10-5
1.702 x 10-5
1.750 x 10-5
1.798 x 10-5
40
1.127
1007
0.02662
1.918 x 10-5
0.7255
1.109
0.02699
1.941 x 10-5
1.963 x 10-5
45
1007
1007
0.7241
50
1.092
0.02735
0.7228
0.02808
0.02881
2.008 x 10-5
2.052 x 10-5
2.096 x 10-5
1.896 x 10-5
1.995 x 10-5
2.097 x 10-5
2.201 x 10-5
60
1.059
1007
0.7202
1.028
0.9994
70
1007
0.7177
0.02953
0.7154
0.7132
80
1008
1008
3.086 x 10-5
3.243 x 10-5
3.565 x 10-5
2.139 x 10-5
2.181 x 10-5
2.264 x 10-5
2.345 x 10-5
90
0.9718
0.03024
100
0.9458
1009
0.03095
2.306 x 10-5
0.7111
120
0.7073
0.7041
0.8977
1011
0.03235
2.522 x 10-5
0.8542
0.8148
2.745 x 10-5
2.975 x 10-5
140
1013
0.03374
3.898 x 10-5
4.241 x 10-5
4.593 x 10-5
4.954 x 10-5
5.890 x 10-5
6.871 x 10-5
7.892 x 10-5
2.420 x 10-5
2.504 x 10-5
2.577 x 10-5
2.760 x 10-5
2.934 x 10-5
160
1016
0.03511
0.7014
180
0.7788
1019
1023
0.03646
3.212 x 10-5
0.6992
200
0.7459
0.03779
3.455 x 10-5
0.6974
0.6746
250
300
1033
0.04104
4.091 x 10-5
0.6946
4.765 x 10-5
5.475 x 10-5
0.6158
1044
0.04418
0.6935
3.101 x 10-5
3.261 x 10-5
3.415 x 10-5
3.563 x 10-5
3.846 x 10-5
350
0.5664
1056
0.04721
0.6937
6.219 x 10-5
6.997 x 10-5
7.806 x 10-5
9.515 x 10-5
8.951 x 10-5
1.004 x 10-4
1.117 x 10-4
1.352 x 10-4
1.598 x 10-4
1.855 x 10-4
2.122 x 10-4
2.398 x 10-4
3.908 x 10-4
5.664 x 10-4
0.6948
0.6965
400
0.5243
1069
0.05015
450
0.4880
1081
0.05298
500
0.4565
1093
0.05572
0.6986
600
0.4042
1115
0.06093
0.7037
4.111 x 10-5
4.362 x 10-5
700
0.3627
1135
0.06581
1.133 x 10-4
0.7092
1.326 x 10-4
1.529 x 10-4
800
0.3289
1153
0.07037
0.7149
900
0.3008
1169
0.07465
4.600 x 10-5
0.7206
1000
1500
4.826 x 10-5
5.817 x 10-5
6.630 x 10-5
0.2772
1184
0.07868
1.741 x 10-4
0.7260
0.09599
2.922 x 10-4
4.270 x 10-4
0.1990
1234
0.7478
2000
0.1553
1264
0.11113
0.7539
Note: For ideal gases, the properties C, k, µ, and Pr are independent of pressure. The properties p, v, and a at a pressure P (in atm) other than 1 atm are determined
by multiplying the values of p at the given temperature by Pand by dividing v and a by P.](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F4447d9cc-345f-4198-8b5a-0a8b631bec55%2F0dd2ecbf-3091-40b4-9758-07608660fba5%2Fudxqzxf_processed.jpeg&w=3840&q=75)
Transcribed Image Text:TABLE A-15
Properties of air at 1 atm pressure
Dynamic
Viscosity
µ, kg/m-s
Kinematic
Prandtl
Specific
Heat
Thermal
Thermal
Temp.
T, °C
Conductivity
k, W/m-K
Density
Diffusivity
Viscosity
v, m?/s
Number
P, kg/m³
Cp, J/kg-K
a, m?/s
Pr
-150
-100
8.636 x 10-6
1.189 x 10-5
2.866
983
0.01171
4.158 x 10-6
3.013 x 10-6
0.7246
8.036 x 10-6
1.252 x 10-5
1.356 x 10-5
1.465 x 10-5
1.578 x 10-5
1.696 x 10-5
2.038
966
0.01582
5.837 x 10-6
0.7263
0.01979
0.02057
-50
1.582
999
1.474 x 10-5
9.319 x 10-6
0.7440
1.527 x 10-5
1.579 x 10-5
1.630 x 10-5
1.680 x 10-5
1.729 x 10-5
1.754 x 10-5
1.778 x 10-5
1.802 x 10-5
1.825 x 10-5
1.849 x 10-5
1.872 x 10-5
-40
-30
1.514
1.451
1002
1004
1.008 x 10-5
1.087 x 10-5
0.7436
0.7425
0.7408
0.02134
0.02211
0.02288
-20
1.394
1005
1.169 x 10-5
-10
1.341
1006
1.252 x 10-5
0.7387
1.292
1006
0.02364
1.818 x 10-5
1.338 x 10-5
0.7362
1.880 x 10-5
1.944 x 10-5
2.009 x 10-5
2.074 x 10-5
2.141 x 10-5
2.208 x 10-5
1.269
1006
0.02401
1.382 x 10-5
0.7350
1.246
1.225
10
1006
0.02439
1.426 x 10-5
0.7336
15
1007
0.02476
1.470 x 10-5
0.7323
1007
1007
1007
1.516 x 10-5
1.562 x 10-5
1.608 x 10-5
1.655 x 10-5
20
1.204
0.02514
0.7309
25
1.184
0.02551
0.7296
30
1.164
0.02588
0.7282
35
1.145
1007
0.02625
2.277 x 10-5
1.895 x 10-5
0.7268
2.346 x 10-5
2.416 x 10-5
2.487 x 10-5
2.632 x 10-5
2.780 x 10-5
2.931 x 10-5
1.702 x 10-5
1.750 x 10-5
1.798 x 10-5
40
1.127
1007
0.02662
1.918 x 10-5
0.7255
1.109
0.02699
1.941 x 10-5
1.963 x 10-5
45
1007
1007
0.7241
50
1.092
0.02735
0.7228
0.02808
0.02881
2.008 x 10-5
2.052 x 10-5
2.096 x 10-5
1.896 x 10-5
1.995 x 10-5
2.097 x 10-5
2.201 x 10-5
60
1.059
1007
0.7202
1.028
0.9994
70
1007
0.7177
0.02953
0.7154
0.7132
80
1008
1008
3.086 x 10-5
3.243 x 10-5
3.565 x 10-5
2.139 x 10-5
2.181 x 10-5
2.264 x 10-5
2.345 x 10-5
90
0.9718
0.03024
100
0.9458
1009
0.03095
2.306 x 10-5
0.7111
120
0.7073
0.7041
0.8977
1011
0.03235
2.522 x 10-5
0.8542
0.8148
2.745 x 10-5
2.975 x 10-5
140
1013
0.03374
3.898 x 10-5
4.241 x 10-5
4.593 x 10-5
4.954 x 10-5
5.890 x 10-5
6.871 x 10-5
7.892 x 10-5
2.420 x 10-5
2.504 x 10-5
2.577 x 10-5
2.760 x 10-5
2.934 x 10-5
160
1016
0.03511
0.7014
180
0.7788
1019
1023
0.03646
3.212 x 10-5
0.6992
200
0.7459
0.03779
3.455 x 10-5
0.6974
0.6746
250
300
1033
0.04104
4.091 x 10-5
0.6946
4.765 x 10-5
5.475 x 10-5
0.6158
1044
0.04418
0.6935
3.101 x 10-5
3.261 x 10-5
3.415 x 10-5
3.563 x 10-5
3.846 x 10-5
350
0.5664
1056
0.04721
0.6937
6.219 x 10-5
6.997 x 10-5
7.806 x 10-5
9.515 x 10-5
8.951 x 10-5
1.004 x 10-4
1.117 x 10-4
1.352 x 10-4
1.598 x 10-4
1.855 x 10-4
2.122 x 10-4
2.398 x 10-4
3.908 x 10-4
5.664 x 10-4
0.6948
0.6965
400
0.5243
1069
0.05015
450
0.4880
1081
0.05298
500
0.4565
1093
0.05572
0.6986
600
0.4042
1115
0.06093
0.7037
4.111 x 10-5
4.362 x 10-5
700
0.3627
1135
0.06581
1.133 x 10-4
0.7092
1.326 x 10-4
1.529 x 10-4
800
0.3289
1153
0.07037
0.7149
900
0.3008
1169
0.07465
4.600 x 10-5
0.7206
1000
1500
4.826 x 10-5
5.817 x 10-5
6.630 x 10-5
0.2772
1184
0.07868
1.741 x 10-4
0.7260
0.09599
2.922 x 10-4
4.270 x 10-4
0.1990
1234
0.7478
2000
0.1553
1264
0.11113
0.7539
Note: For ideal gases, the properties C, k, µ, and Pr are independent of pressure. The properties p, v, and a at a pressure P (in atm) other than 1 atm are determined
by multiplying the values of p at the given temperature by Pand by dividing v and a by P.
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