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{
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"source": [
"# Chapter 10 : Unsteady State And Multidimensional Heat Conduction"
]
},
{
"cell_type": "markdown",
"metadata": {},
"source": [
"## Example 10.8 Page No : 444"
]
},
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"execution_count": 1,
"metadata": {
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"outputs": [
{
"name": "stdout",
"output_type": "stream",
"text": [
"The bottom surface temperature of given slab is 10.3 C\n",
"The top surface temperature of given slab is 19.4 C\n",
"The mid plane temperature of given slab is 12.6 C\n"
]
}
],
"source": [
"# Variables\n",
"l = 0.05 \t\t\t#m,thickness of margarine slab\n",
"ro = 990. \t\t\t#Kg/m**3, density of margarine slab \n",
"cp = 0.55 \t\t\t#Kcal/kg C, ddpecific heat of slab\n",
"k = 0.143 \t\t\t#kcal/h mC, thermal conductivity of slab\n",
"Ti = 4. \t\t\t#C, initial temp\n",
"To = 25. \t\t\t#C, ambient temp.\n",
"t = 4. \t\t\t#hours, time\n",
"h = 8. \t\t\t#kcal/h m**2 C\n",
"\n",
"#calculation\n",
"Fo = k*t/(ro*cp*l**2) \t\t\t#, fourier no.\n",
"Bi = h*l/k \t\t\t#Biot no.\n",
"#from fig. 10.6 a\n",
"Tcbar = 0.7 \t\t\t#Tcbar = (Tc-To)/(Ti-To)\n",
"Tc = To+Tcbar*(Ti-To) \t\t\t#C, centre temp.\n",
"#from fig 10.6 b\n",
"#(T-To)/(Tc-To) = 0.382\n",
"T = 0.382*(Tc-To)+To \t\t\t#c,top surface temp.\n",
"#again from fig. 10.6 b\n",
"Tm = 0.842*(Tc-To)+To \t\t\t#, mid plane temp.\n",
"\n",
"# Results\n",
"print \"The bottom surface temperature of given slab is %.1f C\"%(Tc);\n",
"print \"The top surface temperature of given slab is %.1f C\"%(T);\n",
"print \"The mid plane temperature of given slab is %.1f C\"%(Tm);\n"
]
},
{
"cell_type": "markdown",
"metadata": {},
"source": [
"## Example 10.9 Page No : 449"
]
},
{
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"execution_count": 2,
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{
"name": "stdout",
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"text": [
"i) time required for the cantre-line temp.to drop down to 200 C is 229 s\n",
"ii)the temp. at half radius at that moment is 161 C \n",
"iii)the amount of heat that has been transfered to the liquid is 19647 Kj\n"
]
}
],
"source": [
"import math \n",
"# Variables\n",
"Ti = 870. \t\t\t#C, initial temp.\n",
"To = 30. \t\t\t#C, ambient temp.\n",
"Tc = 200. \t\t\t#C, centre line temp.\n",
"h = 2000. \t\t\t#W/m**2 C, surface heat transfer coefficient\n",
"a = 0.05 \t\t\t#m, radius of cylinder \n",
"k = 20. \t\t\t#W/m C, thermal conductivity\n",
"ro = 7800. \t\t\t#kg/m**3, density\n",
"cp = 0.46*10**3 \t\t\t#j/kg C, specific heat\n",
"\n",
"#calculation\n",
"#i\n",
"Bi = h*a/k \t\t\t#Biot no.\n",
"alpha = k/(ro*cp) \t\t\t#m**2/C, thermal diffusivity\n",
"Tcbar = (Tc-To)/(Ti-To) \t\t\t# dimensionless centre line temp.\n",
"#from fig 10.7 a\n",
"fo = 0.51 \t\t\t#fourier no. fo = alpha*t/a**2\n",
"t = fo*a**2/alpha \t\t\t#s, time\n",
"\n",
"#ii\n",
"#at the half radius, r/a = 0.5 & Bi = 5\n",
"T = To+0.77*(Tc-To) \t\t\t#from fig. 10.7 b\n",
"\n",
"#iii\n",
"x = Bi**2*fo\n",
"#for x = 12.75 & Bi = 5.0. fig.10.9 b gives\n",
"#q/qi = 0.83\n",
"qi = math.pi*a**2*(1)*ro*cp*(Ti-To) \t\t\t#kj, initial amount of heat energy \n",
" #present in 1 m length of shaft\n",
"q = 0.83*qi \t\t\t#j, amount of heat transfered \n",
"\n",
"# Results\n",
"print \"i) time required for the cantre-line temp.to drop down to 200 C is %.0f s\"%(t);\n",
"print \"ii)the temp. at half radius at that moment is %.0f C \"%(T);\n",
"print \"iii)the amount of heat that has been transfered to the liquid is %d Kj\"%(q*10**-3)\n"
]
}
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