diff options
Diffstat (limited to 'Chemical_Engineering_Thermodynamics/ch1.ipynb')
| -rwxr-xr-x | Chemical_Engineering_Thermodynamics/ch1.ipynb | 145 |
1 files changed, 0 insertions, 145 deletions
diff --git a/Chemical_Engineering_Thermodynamics/ch1.ipynb b/Chemical_Engineering_Thermodynamics/ch1.ipynb deleted file mode 100755 index c7a29075..00000000 --- a/Chemical_Engineering_Thermodynamics/ch1.ipynb +++ /dev/null @@ -1,145 +0,0 @@ -{ - "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 |