diff options
Diffstat (limited to 'Chemical_Engineering_Thermodynamics_by_Y_V_C_Rao/ch1.ipynb')
| -rwxr-xr-x | Chemical_Engineering_Thermodynamics_by_Y_V_C_Rao/ch1.ipynb | 145 |
1 files changed, 145 insertions, 0 deletions
diff --git a/Chemical_Engineering_Thermodynamics_by_Y_V_C_Rao/ch1.ipynb b/Chemical_Engineering_Thermodynamics_by_Y_V_C_Rao/ch1.ipynb new file mode 100755 index 00000000..c7a29075 --- /dev/null +++ b/Chemical_Engineering_Thermodynamics_by_Y_V_C_Rao/ch1.ipynb @@ -0,0 +1,145 @@ +{ + "metadata": { + "name": "", + "signature": "sha256:4f7d90cd7b10a2be32d6f9985c84b88b7895b54f53fda509a7ab6972ab90144a" + }, + "nbformat": 3, + "nbformat_minor": 0, + "worksheets": [ + { + "cells": [ + { + "cell_type": "heading", + "level": 1, + "metadata": {}, + "source": [ + "Chapter 1 : Introduction" + ] + }, + { + "cell_type": "heading", + "level": 3, + "metadata": {}, + "source": [ + "Example 1.1 Page No : 6" + ] + }, + { + "cell_type": "code", + "collapsed": false, + "input": [ + "\n", + "\n", + "# Variables\n", + "weight = 981. \t\t\t #weight of payload in N\n", + "gmoon = 1.62;\t\t\t #acceleration due to gravity on the moon in m/s**2\n", + "g = 9.81;\t\t\t #acceleration due to gravity on earth\n", + "\n", + "# Calculations\n", + "mass = weight/g; \t\t\t # Calculations of mass of the payload in kg (calculated as F = m*g)\n", + "weightmoon = mass*gmoon;\t\t\t # Calculations of weight of payload on the moon in N\n", + "\n", + "# Results\n", + "print ' The weight of payload on the moon = %d N'%(weightmoon);\n", + "\n" + ], + "language": "python", + "metadata": {}, + "outputs": [ + { + "output_type": "stream", + "stream": "stdout", + "text": [ + " The weight of payload on the moon = 162 N\n" + ] + } + ], + "prompt_number": 1 + }, + { + "cell_type": "heading", + "level": 3, + "metadata": {}, + "source": [ + "Example 1.2 Page No : 7" + ] + }, + { + "cell_type": "code", + "collapsed": false, + "input": [ + "\n", + "\n", + "# Variables\n", + "l = 15.;\t\t\t #length of the child's head in cm\n", + "b = 12.;\t\t\t #breadth of the child's head in cm\n", + "p = 101325.;\t\t\t #atmospheric pressure in Pa\n", + "\n", + "# Calculations\n", + "area = (l*b)/(10**4);\t\t\t # Calculations of area of the child's head in m**2\n", + "force = p*area;\t\t\t # Calculations of force exerted on the child's head due to atmospheric air in N\n", + "\n", + "# Results\n", + "print ' The force exerted on the childs head due to atmospheric air = %.2f N'%(force);\n", + "\n" + ], + "language": "python", + "metadata": {}, + "outputs": [ + { + "output_type": "stream", + "stream": "stdout", + "text": [ + " The force exerted on the childs head due to atmospheric air = 1823.85 N\n" + ] + } + ], + "prompt_number": 14 + }, + { + "cell_type": "heading", + "level": 3, + "metadata": {}, + "source": [ + "Example 1.3 Page No : 7" + ] + }, + { + "cell_type": "code", + "collapsed": false, + "input": [ + "import math\n", + "\n", + "\n", + "# Variables\n", + "rho_water = 1000.;\t\t\t #density of water flowing through the pipeline in kg/m**3\n", + "rho_manomtr = 1595.;\t\t #density of manometric fluid (carbon tetrachloride) in kg/m**3\n", + "l = 40.;\t \t\t #length between the selected sections in cm\n", + "theta = 45.\t\t\t #inclination of the manometer in degrees\n", + "g = 9.81;\t \t\t #acceleration due to gravity in m/s**2\n", + "\n", + "# Calculations\n", + "delp = (l/100.)*math.sin((theta*math.pi)/180.)*g*(rho_manomtr-rho_water); # Calculations of pressure drop between the required sections in Pa\n", + "\n", + "# Results\n", + "print ' The pressure drop between the required sections = %.2f Pa'%delp\n", + "\n" + ], + "language": "python", + "metadata": {}, + "outputs": [ + { + "output_type": "stream", + "stream": "stdout", + "text": [ + " The pressure drop between the required sections = 1650.94 Pa\n" + ] + } + ], + "prompt_number": 13 + } + ], + "metadata": {} + } + ] +}
\ No newline at end of file |