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{
"metadata": {
"name": "",
"signature": "sha256:0acf769d31306f5bc291e2574308a74de8651b4a4723b52ee59419306e6b7112"
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"nbformat_minor": 0,
"worksheets": [
{
"cells": [
{
"cell_type": "heading",
"level": 1,
"metadata": {},
"source": [
"Chapter 1 : Introduction"
]
},
{
"cell_type": "heading",
"level": 2,
"metadata": {},
"source": [
"Example 1.1 Page No : 20"
]
},
{
"cell_type": "code",
"collapsed": false,
"input": [
"\n",
"# Variables\n",
"d_r = 13640.; \t\t\t# Density of mercury in kg/m3\n",
"g = 9.79; \t\t\t # Acceleration due to gravity in m/s2\n",
"z = 562e-03; \t\t\t# Difference in height in m\n",
"z0 = 761e-03; \t\t\t# Reading of barometer in m\n",
"\n",
"# Calculation\n",
"P = (d_r*g*(z+z0))*(0.987/1e05); \t\t\t# Gas Pressure in bar\n",
"\n",
"# Results\n",
"print \"Gas Pressure is %.3f bar\"%P\n"
],
"language": "python",
"metadata": {},
"outputs": [
{
"output_type": "stream",
"stream": "stdout",
"text": [
"Gas Pressure is 1.744 bar\n"
]
}
],
"prompt_number": 1
},
{
"cell_type": "heading",
"level": 2,
"metadata": {},
"source": [
"Example 1.2 Page No : 21"
]
},
{
"cell_type": "code",
"collapsed": false,
"input": [
"\n",
"# Variables\n",
"d_r = 13.6e03; \t\t\t# Density of mercury in kg/m3\n",
"g = 9.81; \t\t\t# Acceleration due to gravity in m/s2\n",
"z = 710e-03; \t\t\t# Stean flow pressure in m\n",
"z0 = 772e-03; \t\t\t# Reading of barometer in m\n",
"P = 1.4e06; \t\t\t# Gauge pressure of applied steam in Pa\n",
"\n",
"# Calculation\n",
"P0 = d_r*g*z0; \t\t\t# Atmospheric pressure in Pa\n",
"Pi = P+P0 ; \t\t\t# Inlet steam pressure in Pa\n",
"Pc = d_r*g*(z0-z); \t\t\t# Condenser pressure in Pa\n",
"\n",
"# Results\n",
"print \"Inlet steam pressure is %.3e Pa\"%Pi\n",
"print \"Condenser pressure is %.2e Pa\"%Pc\n"
],
"language": "python",
"metadata": {},
"outputs": [
{
"output_type": "stream",
"stream": "stdout",
"text": [
"Inlet steam pressure is 1.503e+06 Pa\n",
"Condenser pressure is 8.27e+03 Pa\n"
]
}
],
"prompt_number": 6
},
{
"cell_type": "heading",
"level": 2,
"metadata": {},
"source": [
"Example 1.3 Page No : 21"
]
},
{
"cell_type": "code",
"collapsed": false,
"input": [
"\n",
"# Variables\n",
"z = 0.760; \t\t\t# Barometer reading in m\n",
"# Part (a)\n",
"h1 = 40e-02; \t\t\t# Mercury height in vaccume in m\n",
"d_r = 13.6e03; \t\t\t# Density of mercury in kg/m3\n",
"g = 9.80; \t\t\t# Acceleration due to gravity in m/s2\n",
"\n",
"# Calculation and Results\n",
"Patm = z*d_r*g; \t\t\t# Atmospheric pressure in Pas\n",
"Pv = h1*d_r*g; \t\t\t# Pressue in vaccume in Pa\n",
"Pabst = Patm-Pv; \t\t\t# Absolute pressure in Pa\n",
"Pabs = 101.325 - Pv/1000\n",
"\n",
"print \"Pvaccum = %.2f kPa\"%(Pv/1000)\n",
"print \"Pabsolute = %.f\"%(Pabst/1000),\"kPa\"\n",
"print \"40 cmHg vacuum : %.3f kPa\"%Pabs\n",
"\n",
"# Part (b)\n",
"h2 = 90e-02; \t\t\t# Mercury height in gauge in m\n",
"Pg = h2*d_r*g; \t\t\t# Gauge Pressure in Pa\n",
"Pabs1 = Patm + Pg ; \t\t\t# Absolute pressure in Pa\n",
"\n",
"print \"\\nPgauge = %.f kPa\"%(Pg/1000)\n",
"print \"90cmHg gauge is %.3f\"%(Pabs1/1000),\"kPa\"\n",
"\n",
"# Part(c)\n",
"d_w = 1e03 ; \t\t\t# Density of water in kg/m3\n",
"h3 = 1.2 ; \t\t\t# Gauge Pressure water height in m\n",
"Pga = d_w*h3*g; \t\t\t# Gauge Pressure in Pa\n",
"Pabs3 = Patm + Pga ; \t\t\t# Absolute pressure in Pa\n",
"print \"\\n1.2 m H2O gauge is %.3f\"%(Pabs3/1000),\"kPa\"\n",
"\n",
"# rounding off error"
],
"language": "python",
"metadata": {},
"outputs": [
{
"output_type": "stream",
"stream": "stdout",
"text": [
"Pvaccum = 53.31 kPa\n",
"Pabsolute = 48 kPa\n",
"40 cmHg vacuum : 48.013 kPa\n",
"\n",
"Pgauge = 120 kPa\n",
"90cmHg gauge is 221.245 kPa\n",
"\n",
"1.2 m H2O gauge is 113.053 kPa\n"
]
}
],
"prompt_number": 3
},
{
"cell_type": "heading",
"level": 2,
"metadata": {},
"source": [
"Example 1.4 Page No : 22"
]
},
{
"cell_type": "code",
"collapsed": false,
"input": [
"from scipy.integrate import quad\n",
"\n",
"# Variables\n",
"Pr = 1.033e05; \t\t\t# Required Pressure in bar\n",
"\n",
"# Calculation\n",
"def pressure(p):\n",
" return p**(-0.714);\n",
"g = 9.81; \t\t\t# Acceleration due to gravity in m/s2\n",
"H = ((2.5e05**0.714)/g)* quad(pressure,0,Pr)[0]; \t\t\t# Depth of atmosphere required in m\n",
"\n",
"# Results\n",
"print \"The depth of atmosphere required is %.3f Km\"%(H/1000)\n",
" \n",
"# note : there will be rounding off error because of quad function"
],
"language": "python",
"metadata": {},
"outputs": [
{
"output_type": "stream",
"stream": "stdout",
"text": [
"The depth of atmosphere required is 69.203 Km\n"
]
}
],
"prompt_number": 23
},
{
"cell_type": "heading",
"level": 2,
"metadata": {},
"source": [
"Example 1.5 Page No : 22"
]
},
{
"cell_type": "code",
"collapsed": false,
"input": [
"\n",
"# Variables\n",
"m = 68. ; \t\t\t# Astronaut mass in Kg\n",
"g = 9.806; \t\t\t# Acceleration due to gravity in m/s2\n",
"\n",
"# Calculation\n",
"a = 10*g ; \t\t\t# Lift off acceleration in m/s2\n",
"F = m*a; \t\t\t# Net vertical force in N\n",
"\n",
"# Results\n",
"print \"Net vertical force experienced by astronaut is %.0f N\"%F\n"
],
"language": "python",
"metadata": {},
"outputs": [
{
"output_type": "stream",
"stream": "stdout",
"text": [
"Net vertical force experienced by astronaut is 6668 N\n"
]
}
],
"prompt_number": 6
}
],
"metadata": {}
}
]
}
|
