diff options
author | Trupti Kini | 2017-03-17 23:30:25 +0600 |
---|---|---|
committer | Trupti Kini | 2017-03-17 23:30:25 +0600 |
commit | 2a5f1f9f2af82c46fbdba902c9dfdaba56c136b0 (patch) | |
tree | 7ce76ec82cb74706a939781d9bf0c7c9afab53e5 /Introduction_to_Heat_Transfer_by_S._K._Som/Chapter6.ipynb | |
parent | d93e64cd264d30ae87de69ab9ab7f377d6047361 (diff) | |
download | Python-Textbook-Companions-2a5f1f9f2af82c46fbdba902c9dfdaba56c136b0.tar.gz Python-Textbook-Companions-2a5f1f9f2af82c46fbdba902c9dfdaba56c136b0.tar.bz2 Python-Textbook-Companions-2a5f1f9f2af82c46fbdba902c9dfdaba56c136b0.zip |
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.ipynb | 102 |
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" ] } ], |