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diff --git a/Machine_Design_by_U.C._Jindal/Ch5.ipynb b/Machine_Design_by_U.C._Jindal/Ch5.ipynb new file mode 100644 index 00000000..ea122295 --- /dev/null +++ b/Machine_Design_by_U.C._Jindal/Ch5.ipynb @@ -0,0 +1,253 @@ +{ + "metadata": { + "name": "", + "signature": "sha256:56bbd90f35decd7f62fabe45fb918c0e397bbdcedfeeda130ab611b764281c1a" + }, + "nbformat": 3, + "nbformat_minor": 0, + "worksheets": [ + { + "cells": [ + { + "cell_type": "heading", + "level": 1, + "metadata": {}, + "source": [ + "Ch:5 Introduction to pressure vessels" + ] + }, + { + "cell_type": "heading", + "level": 2, + "metadata": {}, + "source": [ + "exa 5-1 - Page 138" + ] + }, + { + "cell_type": "code", + "collapsed": false, + "input": [ + "p=2#\n", + "Rm=220#\n", + "#tensile hoop or circumferential stress= sigt\n", + "sigr=-2#\n", + "#sigt=(p*Rm)/t#\n", + "Sa=230/2#\n", + "#t1=thickness according to maximum principal stress theory\n", + "#t2=thickness according to maximum shear stress theory\n", + "t1=(p*Rm)/Sa#\n", + "t2=(p*Rm)/(Sa+sigr)#\n", + "print \"t1 is %0.2f mm \"%(t1)#\n", + "print \"\\nt2 is %0.3f mm \"%(t2)#" + ], + "language": "python", + "metadata": {}, + "outputs": [ + { + "output_type": "stream", + "stream": "stdout", + "text": [ + "t1 is 3.00 mm \n", + "\n", + "t2 is 3.000 mm \n" + ] + } + ], + "prompt_number": 1 + }, + { + "cell_type": "heading", + "level": 2, + "metadata": {}, + "source": [ + "exa 5-2 - Page 139" + ] + }, + { + "cell_type": "code", + "collapsed": false, + "input": [ + "from math import sqrt\n", + "from __future__ import division\n", + "#Elastic limit=sige\n", + "sige=310#\n", + "#inside diameter=di\n", + "di=300#\n", + "p=1.8#\n", + "FOS=2#\n", + "#design stress=sigd#\n", + "sigd=sige/2#\n", + "c=0.162#\n", + "d=380#\n", + "#cover plate thickness=t#\n", + "t=d*sqrt(c*p/sigd)#\n", + "t=17#\n", + "M=di*p*t/4#\n", + "\n", + "z=(1/6)*1*t**2#\n", + "#bending stress=sigb#\n", + "sigb=M/z#\n", + "print \"t is %0.1fmm \"%(t)#\n", + "print \"\\nM is %0.1fmm \"%(M)#\n", + "print \"\\nsigb is %0.1fmm \"%(sigb)#\n", + "if (sigb<=sigd):\n", + " print 'sigb is below allowable sigd.'" + ], + "language": "python", + "metadata": {}, + "outputs": [ + { + "output_type": "stream", + "stream": "stdout", + "text": [ + "t is 17.0mm \n", + "\n", + "M is 2295.0mm \n", + "\n", + "sigb is 47.6mm \n", + "sigb is below allowable sigd.\n" + ] + } + ], + "prompt_number": 2 + }, + { + "cell_type": "heading", + "level": 2, + "metadata": {}, + "source": [ + "exa 5-3 - Page 140" + ] + }, + { + "cell_type": "code", + "collapsed": false, + "input": [ + "sige=220#\n", + "v=0.29#\n", + "Ri=175#\n", + "FOS=3#\n", + "Sa=sige/3#\n", + "p=10#\n", + "#t1=thickness according to maximum principal stress theory\n", + "#t2=thickness according to maximum shear stress theory\n", + "x=Sa+(p*(1-(2*v)))#\n", + "y=Sa-(p*(1+v))#\n", + "t1=(sqrt(x/y)-1)*Ri#\n", + "t1=24#\n", + "#t1=((sqrt((Sa+(p*(1-(2*v)))))/(Sa-(p*(1+v))))-1)*Ri#\n", + "t2=Ri*((sqrt(Sa/(Sa-(2*p))))-1)#\n", + "# printing data in scilab o/p window\n", + "print \"t1 is %0.1fmm \"%(t1)#\n", + "print \"\\nt2 is %0.3fmm \"%(t2)#\n", + "#The answer to t2 is not calculated in the book." + ], + "language": "python", + "metadata": {}, + "outputs": [ + { + "output_type": "stream", + "stream": "stdout", + "text": [ + "t1 is 24.0mm \n", + "\n", + "t2 is 30.206mm \n" + ] + } + ], + "prompt_number": 3 + }, + { + "cell_type": "heading", + "level": 2, + "metadata": {}, + "source": [ + "exa 5-4 - Page 141" + ] + }, + { + "cell_type": "code", + "collapsed": false, + "input": [ + "p=16#\n", + "Ri=250#\n", + "#Yield strength =sigy#\n", + "sigy=330#\n", + "v=0.3#\n", + "FOS=3#\n", + "Sa=sigy/3#\n", + "t=Ri*((sqrt(Sa/(Sa-(2*p))))-1)#\n", + "t=50#\n", + "\n", + "print \"t is %0.1fmm \"%(t)#" + ], + "language": "python", + "metadata": {}, + "outputs": [ + { + "output_type": "stream", + "stream": "stdout", + "text": [ + "t is 50.0mm \n" + ] + } + ], + "prompt_number": 4 + }, + { + "cell_type": "heading", + "level": 2, + "metadata": {}, + "source": [ + "exa 5-5 - Page 141" + ] + }, + { + "cell_type": "code", + "collapsed": false, + "input": [ + "from math import pi\n", + "d=15#\n", + "Eg=480#\n", + "t=3#\n", + "#flange thickness=ft#\n", + "ft=12#\n", + "A=pi*d**2/4#\n", + "l=d+t+(ft/2)#\n", + "E=210#\n", + "kb=A*E/l#\n", + "#effective area of gasket=Ag#\n", + "Ag=pi*(((ft+t+d)**2)-(d**2))/4#\n", + "kg=Ag*Eg/t#\n", + "# printing data in scilab o/p window\n", + "print \"kb is %0.3f N/mm \"%(kb)#\n", + "kb=kb*10**-3#\n", + "kg=kg*10**-3#\n", + "if (kb<=kg):\n", + " print \"\\nThe combines stiffness of bolt and gasket is %0.3f kN/mm\"%(kg)\n", + "\n", + "\n", + "#The difference in the value of kb is due to rounding-off the value of A \n", + " " + ], + "language": "python", + "metadata": {}, + "outputs": [ + { + "output_type": "stream", + "stream": "stdout", + "text": [ + "kb is 1546.253 N/mm \n", + "\n", + "The combines stiffness of bolt and gasket is 84.823 kN/mm\n" + ] + } + ], + "prompt_number": 5 + } + ], + "metadata": {} + } + ] +}
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