Elements Of Electromagnetics
Elements Of Electromagnetics
7th Edition
ISBN: 9780190698614
Author: Sadiku, Matthew N. O.
Publisher: Oxford University Press
Bartleby Related Questions Icon

Related questions

bartleby

Concept explainers

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.
expand button
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.
expand button
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.
Expert Solution
Check Mark
Knowledge Booster
Background pattern image
Mechanical Engineering
Learn more about
Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, mechanical-engineering and related others by exploring similar questions and additional content below.
Similar questions
Recommended textbooks for you
Text book image
Elements Of Electromagnetics
Mechanical Engineering
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Oxford University Press
Text book image
Mechanics of Materials (10th Edition)
Mechanical Engineering
ISBN:9780134319650
Author:Russell C. Hibbeler
Publisher:PEARSON
Text book image
Thermodynamics: An Engineering Approach
Mechanical Engineering
ISBN:9781259822674
Author:Yunus A. Cengel Dr., Michael A. Boles
Publisher:McGraw-Hill Education
Text book image
Control Systems Engineering
Mechanical Engineering
ISBN:9781118170519
Author:Norman S. Nise
Publisher:WILEY
Text book image
Mechanics of Materials (MindTap Course List)
Mechanical Engineering
ISBN:9781337093347
Author:Barry J. Goodno, James M. Gere
Publisher:Cengage Learning
Text book image
Engineering Mechanics: Statics
Mechanical Engineering
ISBN:9781118807330
Author:James L. Meriam, L. G. Kraige, J. N. Bolton
Publisher:WILEY