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authorTrupti Kini2017-03-17 23:30:25 +0600
committerTrupti Kini2017-03-17 23:30:25 +0600
commit2a5f1f9f2af82c46fbdba902c9dfdaba56c136b0 (patch)
tree7ce76ec82cb74706a939781d9bf0c7c9afab53e5 /Introduction_to_Heat_Transfer_by_S._K._Som/Chapter6.ipynb
parentd93e64cd264d30ae87de69ab9ab7f377d6047361 (diff)
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Added(A)/Deleted(D) following books
M Introduction_to_Heat_Transfer_by_S._K._Som/Chapter1.ipynb M Introduction_to_Heat_Transfer_by_S._K._Som/Chapter10.ipynb M Introduction_to_Heat_Transfer_by_S._K._Som/Chapter11.ipynb M Introduction_to_Heat_Transfer_by_S._K._Som/Chapter2.ipynb M Introduction_to_Heat_Transfer_by_S._K._Som/Chapter3.ipynb M Introduction_to_Heat_Transfer_by_S._K._Som/Chapter4.ipynb M Introduction_to_Heat_Transfer_by_S._K._Som/Chapter5.ipynb M Introduction_to_Heat_Transfer_by_S._K._Som/Chapter6.ipynb M Introduction_to_Heat_Transfer_by_S._K._Som/Chapter7.ipynb M Introduction_to_Heat_Transfer_by_S._K._Som/Chapter8.ipynb M Introduction_to_Heat_Transfer_by_S._K._Som/Chapter9.ipynb M Introduction_to_Heat_Transfer_by_S._K._Som/chapter12.ipynb
Diffstat (limited to 'Introduction_to_Heat_Transfer_by_S._K._Som/Chapter6.ipynb')
-rw-r--r--Introduction_to_Heat_Transfer_by_S._K._Som/Chapter6.ipynb102
1 files changed, 7 insertions, 95 deletions
diff --git a/Introduction_to_Heat_Transfer_by_S._K._Som/Chapter6.ipynb b/Introduction_to_Heat_Transfer_by_S._K._Som/Chapter6.ipynb
index a4433df7..5a31da63 100644
--- a/Introduction_to_Heat_Transfer_by_S._K._Som/Chapter6.ipynb
+++ b/Introduction_to_Heat_Transfer_by_S._K._Som/Chapter6.ipynb
@@ -18,7 +18,7 @@
},
{
"cell_type": "code",
- "execution_count": 3,
+ "execution_count": 10,
"metadata": {
"collapsed": false
},
@@ -45,7 +45,6 @@
}
],
"source": [
- " \n",
"import math\n",
" \n",
"print\"Introduction to heat transfer by S.K.Som, Chapter 6, Example 1\"\n",
@@ -55,7 +54,7 @@
"mu=0.1;\n",
"b=0.005; #in metre\n",
" #Umax is maximum velocity\n",
- " Umax=(3.0/2)*Uav\n",
+ " Umax=(3/2)*Uav\n",
"print\"Umax in m/s is\"\n",
"Umax=(3/2)*Uav\n",
"print\"Umax=\",Umax\n",
@@ -82,31 +81,7 @@
" #Since pressure drop is considered at a distance of 2m so L=2m\n",
"L=2;\n",
"deltaP=(-X)*L\n",
- "print\"deltaP=\",deltaP\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n"
+ "print\"deltaP=\",deltaP"
]
},
{
@@ -118,7 +93,7 @@
},
{
"cell_type": "code",
- "execution_count": 2,
+ "execution_count": 14,
"metadata": {
"collapsed": false
},
@@ -138,7 +113,6 @@
}
],
"source": [
- " \n",
"import math\n",
" \n",
"print\"Introduction to heat transfer by S.K.Som, Chapter 6, Example 3\"\n",
@@ -159,28 +133,7 @@
" #The viscosity of oil is mu=(pi*D**4*X)/(128*Q*dz)\n",
"print\"The viscosity of oil(mu)in kg/(m*s)\"\n",
"mu=(math.pi*D**4*X)/(128*Q)\n",
- "print\"mu=\",mu\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n"
+ "print\"mu=\",mu"
]
},
{
@@ -212,10 +165,6 @@
}
],
"source": [
- " \n",
- " \n",
- " \n",
- " \n",
"import math\n",
" \n",
"print\"Introduction to heat transfer by S.K.Som, Chapter 6, Example 7\"\n",
@@ -239,26 +188,7 @@
" #Fd is drag force\n",
"print\"Drag force on one side of plate in N is\"\n",
"Fd=cfL*(rhoair*Uinf**2/2)*B*L\n",
- "print\"Fd=\",Fd\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n"
+ "print\"Fd=\",Fd"
]
},
{
@@ -294,10 +224,6 @@
}
],
"source": [
- " \n",
- " \n",
- " \n",
- " \n",
"import math\n",
" \n",
"print\"Introduction to heat transfer by S.K.Som, Chapter 6, Example 10\"\n",
@@ -326,21 +252,7 @@
" #The turbulent boundary layer thickness at the trailing edge is given by delta=L*(0.379/ReL**(1/5))\n",
"print\"The turbulent boundary layer thickness at the trailing edge in metre is \"\n",
"delta=L*(0.379/ReL**(1/5))\n",
- "print\"delta=\",delta\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n",
- "\n"
+ "print\"delta=\",delta"
]
}
],