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author | Trupti Kini | 2016-01-11 23:30:05 +0600 |
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committer | Trupti Kini | 2016-01-11 23:30:05 +0600 |
commit | 8fa3a985b0772b28f8e6e6f5aec18bca1c0f7332 (patch) | |
tree | 5a9269d094b4a98947094c7c23cee3dbb3ae6c68 /Engineering_Mechanics_of_Solids_by_Popov_E_P/chapter5.ipynb | |
parent | e1dbc4e45afcfcd26275010a9c0008b5d7f7e5ea (diff) | |
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Added(A)/Deleted(D) following books
A Engineering_Mechanics_of_Solids_by_Popov_E_P/Chapter1.ipynb
A Engineering_Mechanics_of_Solids_by_Popov_E_P/chapter10.ipynb
A Engineering_Mechanics_of_Solids_by_Popov_E_P/chapter11.ipynb
A Engineering_Mechanics_of_Solids_by_Popov_E_P/chapter12.ipynb
A Engineering_Mechanics_of_Solids_by_Popov_E_P/chapter2.ipynb
A Engineering_Mechanics_of_Solids_by_Popov_E_P/chapter4.ipynb
A Engineering_Mechanics_of_Solids_by_Popov_E_P/chapter5.ipynb
A Engineering_Mechanics_of_Solids_by_Popov_E_P/chapter6.ipynb
A Engineering_Mechanics_of_Solids_by_Popov_E_P/chapter7.ipynb
A Engineering_Mechanics_of_Solids_by_Popov_E_P/chapter8.ipynb
A Engineering_Mechanics_of_Solids_by_Popov_E_P/chapter9.ipynb
A Engineering_Mechanics_of_Solids_by_Popov_E_P/charpter_3.ipynb
A Engineering_Mechanics_of_Solids_by_Popov_E_P/charpter_3_1.ipynb
A Engineering_Mechanics_of_Solids_by_Popov_E_P/screenshots/Untitled.png
A Engineering_Mechanics_of_Solids_by_Popov_E_P/screenshots/cap2.png
A Engineering_Mechanics_of_Solids_by_Popov_E_P/screenshots/cap3.png
A Microwave_Engineering_by_G._S._Raghuvanshi/Ch1.ipynb
A Microwave_Engineering_by_G._S._Raghuvanshi/Ch10.ipynb
A Microwave_Engineering_by_G._S._Raghuvanshi/Ch11.ipynb
A Microwave_Engineering_by_G._S._Raghuvanshi/Ch12.ipynb
A Microwave_Engineering_by_G._S._Raghuvanshi/Ch2.ipynb
A Microwave_Engineering_by_G._S._Raghuvanshi/Ch3.ipynb
A Microwave_Engineering_by_G._S._Raghuvanshi/Ch4.ipynb
A Microwave_Engineering_by_G._S._Raghuvanshi/Ch5.ipynb
A Microwave_Engineering_by_G._S._Raghuvanshi/Ch6.ipynb
A Microwave_Engineering_by_G._S._Raghuvanshi/Ch7.ipynb
A Microwave_Engineering_by_G._S._Raghuvanshi/Ch8.ipynb
A Microwave_Engineering_by_G._S._Raghuvanshi/Ch9.ipynb
A Microwave_Engineering_by_G._S._Raghuvanshi/screenshots/12refCoeff.png
A Microwave_Engineering_by_G._S._Raghuvanshi/screenshots/1RefCoeff.png
A Microwave_Engineering_by_G._S._Raghuvanshi/screenshots/6axialPhasVel.png
Diffstat (limited to 'Engineering_Mechanics_of_Solids_by_Popov_E_P/chapter5.ipynb')
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diff --git a/Engineering_Mechanics_of_Solids_by_Popov_E_P/chapter5.ipynb b/Engineering_Mechanics_of_Solids_by_Popov_E_P/chapter5.ipynb new file mode 100644 index 00000000..089d0b85 --- /dev/null +++ b/Engineering_Mechanics_of_Solids_by_Popov_E_P/chapter5.ipynb @@ -0,0 +1,870 @@ +{
+ "metadata": {
+ "name": "",
+ "signature": "sha256:71148b069e338fd0ffabcfe7f6bd37d7ab47477a297f58633926ede4f66ab53c"
+ },
+ "nbformat": 3,
+ "nbformat_minor": 0,
+ "worksheets": [
+ {
+ "cells": [
+ {
+ "cell_type": "heading",
+ "level": 2,
+ "metadata": {},
+ "source": [
+ "Chapter 5:Axial force, Shear and Bending moment "
+ ]
+ },
+ {
+ "cell_type": "heading",
+ "level": 2,
+ "metadata": {},
+ "source": [
+ "Example5.2 pagenumber 231"
+ ]
+ },
+ {
+ "cell_type": "code",
+ "collapsed": false,
+ "input": [
+ "#Given \n",
+ "L_ab = 0.4 #mt The total length of the rod\n",
+ "M = 200 #N_m - the moment acting on rod\n",
+ "l_1 = 0.1 #mt -moment acting point the distance from 'a'\n",
+ "R_1 = 100 #N - The Force acting \n",
+ "l_2 = 0.2 #mt -R_1 acting point the distance from 'a'\n",
+ "R_2 = 160 #N The Force acting \n",
+ "l_3 = 0.3 #mt -R_2 acting point the distance from 'a'\n",
+ "#caliculations\n",
+ "\n",
+ "#F_X = 0 forces in x directions \n",
+ "R_A_X = 0 # since there are no forces in X-direction \n",
+ "R_B_X = 0\n",
+ "#M_A = 0 momentum at point a is zero\n",
+ "\n",
+ "# M + R_1*l_2 + R_2*l_3 = R_B*L_ab *the moment for a force is FxL\n",
+ "R_B_Y = (M + R_1*l_2 + R_2*l_3)/L_ab\n",
+ "\n",
+ "#M_B= 0 momentum at point b is zero\n",
+ "# R_A_Y*L_ab + M - R_1*l_2 - R_2*0.1 = 0\n",
+ "\n",
+ "R_A_Y = -(M - R_1*l_2 - R_2*0.1)/L_ab\n",
+ " \n",
+ "print \"The X,Y components of reaction force at A is \",R_A_X,\",\",R_A_Y,\"N\"\n",
+ "print \"The X,Y components of reaction force at B is \",R_B_X,\",\",R_B_Y,\"N\""
+ ],
+ "language": "python",
+ "metadata": {},
+ "outputs": [
+ {
+ "output_type": "stream",
+ "stream": "stdout",
+ "text": [
+ "The X,Y components of reaction force at A is 0 , -410.0 N\n",
+ "The X,Y components of reaction force at B is 0 , 670.0 N\n"
+ ]
+ }
+ ],
+ "prompt_number": 8
+ },
+ {
+ "cell_type": "heading",
+ "level": 2,
+ "metadata": {},
+ "source": [
+ "Example 5.2 page number 233"
+ ]
+ },
+ {
+ "cell_type": "code",
+ "collapsed": false,
+ "input": [
+ "#Given \n",
+ "P_Max = 10 #N - the maximum distribution in a triangular distribution\n",
+ "L = 3 #mt the total length of force distribution \n",
+ "L_X = 5 #mt - the horizantal length of the rod\n",
+ "#caliculations \n",
+ "\n",
+ "F_y = P_Max*L*0.5 #N - The force due to triangular distribition \n",
+ "L_com = 2*L /3 #mt - the resultant force acting as a result of distribution acting position \n",
+ "#F_X = 0 forces in x directions\n",
+ "R_A_X = 0 # since there are no forces in X-direction\n",
+ "R_B_X = 0\n",
+ "#M_A = 0 momentum at point a is zero\n",
+ "#F_y*L_com - R_B_Y*L_X = 0\n",
+ "R_B_Y = F_y*L_com/L_X\n",
+ "\n",
+ "#M_B= 0 momentum at point b is zero\n",
+ "#- R_A_Y*L_X = F_y*(L_X-L )\n",
+ "\n",
+ "R_A_Y = - F_y*L/L_X \n",
+ "print \"The X,Y components of reaction force at A is \",R_A_X,\",\",R_A_Y,\"N\"\n",
+ "print \"The X,Y components of reaction force at B is \",R_B_X,\",\",R_B_Y,\"N\"\n"
+ ],
+ "language": "python",
+ "metadata": {},
+ "outputs": [
+ {
+ "output_type": "stream",
+ "stream": "stdout",
+ "text": [
+ "The X,Y components of reaction force at A is 0 , -9.0 N\n",
+ "The X,Y components of reaction force at B is 0 , 6.0 N\n"
+ ]
+ }
+ ],
+ "prompt_number": 9
+ },
+ {
+ "cell_type": "heading",
+ "level": 2,
+ "metadata": {},
+ "source": [
+ "\n",
+ "Example 5.3 page number 233\n",
+ "\n",
+ "\n",
+ "\n"
+ ]
+ },
+ {
+ "cell_type": "code",
+ "collapsed": false,
+ "input": [
+ "#given\n",
+ "F = 5 #K - force acting on the system\n",
+ "tan = (4/3) # the Tan of the angle of force with x axis\n",
+ "l_ab = 12 #inch - the total length of ab \n",
+ "l = 3 # inch - Distance from 'a'\n",
+ "#caliculation\n",
+ "F_X = 4 #K\n",
+ "F_Y = 3 #k\n",
+ "\n",
+ "#M_A = 0 momentum at point a is zero\n",
+ "# F_X*l- R_B_Y*l_ab = 0 \n",
+ "R_B_Y = F_X*l/l_ab\n",
+ "\n",
+ "#M_B= 0 momentum at point b is zero\n",
+ "# R_A_Y*l_ab - F_X*(l_ab - l)\n",
+ "R_A_Y = F_X*(l_ab - l)/l_ab\n",
+ " \n",
+ "#F_X = 0 forces in x directions\n",
+ "R_A_X = F_Y + R_B_Y \n",
+ "R_B_X = R_B_Y # since the angle is 45 degrees\n",
+ "\n",
+ "#resultants \n",
+ "R_A = pow(R_A_X**2 + R_A_Y**2,0.5)\n",
+ "R_B = pow(R_B_X**2 + R_B_Y**2,0.5)\n",
+ "\n",
+ "print \"The X,Y components and resultant of reaction force at A is \",R_A_X,\",\",R_A_Y,\",\",R_A,\"N\"\n",
+ "print \"The X,Y components and resultant of reaction force at B is \",R_B_X,\",\",R_B_Y,\",\",round(R_B,2),\"N\"\n",
+ "\n"
+ ],
+ "language": "python",
+ "metadata": {},
+ "outputs": [
+ {
+ "output_type": "stream",
+ "stream": "stdout",
+ "text": [
+ "The X,Y components and resultant of reaction force at A is 4 , 3 , 5.0 N\n",
+ "The X,Y components and resultant of reaction force at B is 1 , 1 , 1.41 N\n"
+ ]
+ }
+ ],
+ "prompt_number": 11
+ },
+ {
+ "cell_type": "heading",
+ "level": 2,
+ "metadata": {},
+ "source": [
+ "Example 5.4 page number 239"
+ ]
+ },
+ {
+ "cell_type": "code",
+ "collapsed": false,
+ "input": [
+ "#Given \n",
+ "P_Max = 10 #N - the maximum distribution in a triangular distribution\n",
+ "L = 3 #mt the total length of force distribution \n",
+ "L_X = 5 #mt - the horizantal length of the rod\n",
+ "#caliculations \n",
+ "\n",
+ "F_y = P_Max*L*0.5 #N - The force due to triangular distribition \n",
+ "L_com = 2*L /3 #mt - the resultant force acting as a result of distribution acting position \n",
+ "#F_X = 0 forces in x directions\n",
+ "R_A_X = 0 # since there are no forces in X-direction\n",
+ "R_B_X = 0\n",
+ "#M_A = 0 momentum at point a is zero\n",
+ "#F_y*L_com - R_B_Y*L_X = 0\n",
+ "R_B_Y = F_y*L_com/L_X\n",
+ "\n",
+ "#M_B= 0 momentum at point b is zero\n",
+ "#- R_A_Y*L_X = F_y*(L_X-L )\n",
+ "\n",
+ "R_A_Y = - F_y*L/L_X\n",
+ "\n",
+ "#For a---a section \n",
+ "l_a = 2 #mt - a---a section from a \n",
+ "l_com_a = 2*l_a/3\n",
+ "v_a = R_A_Y + 0.5*l_a*(10.0*2/3) #*(10*2/3) because the maximum moves\n",
+ "\n",
+ "M_a = (10.0*0.66)*l_a*(0.33) + R_A_Y*l_a \n",
+ "\n",
+ "#For b---b section \n",
+ "\n",
+ "v_b = F_y + R_A_Y #equilabrium conditions\n",
+ "M_b = (F_Y + R_A_Y)*(-1)\n",
+ "\n",
+ "print \"The force and moment in section a--a are\",round(v_a,2),\"KN ,\",M_a,\"KN-m\"\n",
+ "print \"The force and moment in section b--b are\",v_b,\"KN ,\",M_b,\"KN-m\""
+ ],
+ "language": "python",
+ "metadata": {},
+ "outputs": [
+ {
+ "output_type": "stream",
+ "stream": "stdout",
+ "text": [
+ "The force and moment in section a--a are -2.33 KN , -13.644 KN-m\n",
+ "The force and moment in section b--b are 6.0 KN , 6.0 KN-m\n"
+ ]
+ }
+ ],
+ "prompt_number": 34
+ },
+ {
+ "cell_type": "heading",
+ "level": 2,
+ "metadata": {},
+ "source": [
+ "Example 5.5 page number 241"
+ ]
+ },
+ {
+ "cell_type": "code",
+ "collapsed": false,
+ "input": [
+ "#Given \n",
+ "#Lets divide the section into two sections \n",
+ "l_ac = 10 # ft -The total length of the rod\n",
+ "R = 5 #k - The applies force at c\n",
+ "tan = 4/3 # The tan of the angle of the force \n",
+ "l_ab = 5 #ft - The distance of applied force from A\n",
+ "R_y = 4 #k,downwards X- component of the force\n",
+ "R_X = 3 #k Y- component of the force , lets consider only Y direction since we are concentrating on the Shears \n",
+ "\n",
+ "#F_Y = 0 forces in Y directions\n",
+ "#R_A +R_B = R_y\n",
+ "#M_c = 0 making the moment zero at point c \n",
+ "#Caliculations \n",
+ "# R_A= R_B*(l_ac - l_ab)/(l_ab) so R_A = R_B\n",
+ "\n",
+ "R_A = R_y/2 #F_Y = 0\n",
+ "R_B = R_y/2\n",
+ "#considering section x--x\n",
+ "l_x = 2 #ft - length of section from A\n",
+ "v_x = R_A #k ,F_X = 0 \n",
+ "M_x = R_A*l_x #k-ft M_c = 0\n",
+ "\n",
+ "#considering section at midpoint t--t\n",
+ "l_t = 2 #ft - length of section from A\n",
+ "v_t = 0 #k ,F_X = 0 \n",
+ "M_t = (R_A)*l_t #k-ft M_c = 0\n",
+ "\n",
+ "##considering section y---y\n",
+ "l_y = 2 #ft - length of section from B\n",
+ "v_y = - R_B #k ,F_X = 0 \n",
+ "M_y = R_B*l_y #k-ft M_c = 0\n",
+ "\n",
+ "#Graph\n",
+ "%matplotlib inline\n",
+ "import math \n",
+ "from matplotlib.pyplot import plot,suptitle,xlabel,ylabel\n",
+ "#Drawing of shear and bending moment diagram\n",
+ "print \"Given problem is for drawing diagram, this diagram is drawn by step by step manner. \"\n",
+ "X = [0,2,4.9999999999999,5,5.00000000000000001,7,10] # For graph precision \n",
+ "\n",
+ "V = [R_A,v_x,v_x,v_t,v_y,v_y,-R_B];\t\t\t#Shear matrix\n",
+ "M = [0,M_x,M_t,M_t,M_t,M_y,0];\t\t\t#Bending moment matrix\n",
+ "plot(X,V);\t\t\t#Shear diagram\n",
+ "plot(X,M,'r');\t\t\t#Bending moment diagram\n",
+ "suptitle( 'Shear and bending moment diagram')\n",
+ "xlabel('X axis')\n",
+ "ylabel( 'Y axis') ;"
+ ],
+ "language": "python",
+ "metadata": {},
+ "outputs": [
+ {
+ "output_type": "stream",
+ "stream": "stdout",
+ "text": [
+ "Given problem is for drawing diagram, this diagram is drawn by step by step manner. \n"
+ ]
+ },
+ {
+ "metadata": {},
+ "output_type": "display_data",
+ "png": 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+ "text": [
+ "<matplotlib.figure.Figure at 0x87a5ac8>"
+ ]
+ }
+ ],
+ "prompt_number": 42
+ },
+ {
+ "cell_type": "heading",
+ "level": 2,
+ "metadata": {},
+ "source": [
+ "Example 5.6 pagenumber 243 "
+ ]
+ },
+ {
+ "cell_type": "code",
+ "collapsed": false,
+ "input": [
+ "#Given\n",
+ "l = 1 #L - Length of the cantilever \n",
+ "F_app = ((2**0.5))*2 #p - force applies \n",
+ "tan = 1 # The angle of force applied\n",
+ "F_app_x = F_app/((2**0.5)) #p The horizantal component of the force , neglected \n",
+ "F_app_y = F_app/((2**0.5)) #p The Vertical component of the force \n",
+ "#F_Y = 0 \n",
+ "R_A = 1 #p\n",
+ "\n",
+ "#Considering section 1-----1\n",
+ "l_1 = 0.5 # The length of the section from one end\n",
+ "v_1 = R_A #F_Y = 0\n",
+ "M_1 = -R_A*l_1 #MAking moment at section 1 = 0\n",
+ "\n",
+ "#considering end of cantilever\n",
+ "l_2 = 1 # The length of the section from one end\n",
+ "v_2 = R_A #F_Y = 0\n",
+ "M_2 = -R_A*l_2#MAking moment at section 1 = 0\n",
+ "\n",
+ "#Graph\n",
+ "%matplotlib inline\n",
+ "import math \n",
+ "from matplotlib.pyplot import plot,suptitle,xlabel,ylabel\n",
+ "#Drawing of shear and bending moment diagram\n",
+ "print \"Given problem is for drawing diagram, this diagram is drawn by step by step manner. \"\n",
+ "X = [0,0.5,1] # For graph precision \n",
+ "\n",
+ "V = [R_A,v_1,v_2 ];\t\t\t#Shear matrix\n",
+ "M = [0,M_1,M_2];\t\t\t#Bending moment matrix\n",
+ "plot(X,V);\t\t\t #Shear diagram\n",
+ "plot(X,M,'r');\t\t\t #Bending moment diagram\n",
+ "suptitle( 'Shear and bending moment diagram')\n",
+ "xlabel('X axis')\n",
+ "ylabel( 'Y axis') ;\n",
+ "\n",
+ "\n",
+ "\n",
+ "\n",
+ "\n"
+ ],
+ "language": "python",
+ "metadata": {},
+ "outputs": [
+ {
+ "output_type": "stream",
+ "stream": "stdout",
+ "text": [
+ "Given problem is for drawing diagram, this diagram is drawn by step by step manner. \n"
+ ]
+ },
+ {
+ "metadata": {},
+ "output_type": "display_data",
+ "png": 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+ "text": [
+ "<matplotlib.figure.Figure at 0x8154208>"
+ ]
+ }
+ ],
+ "prompt_number": 128
+ },
+ {
+ "cell_type": "heading",
+ "level": 2,
+ "metadata": {},
+ "source": [
+ "Example 5.7 page number 243"
+ ]
+ },
+ {
+ "cell_type": "code",
+ "collapsed": false,
+ "input": [
+ "#Given\n",
+ "l_ab = 3 #L - The total length lets say '3L'\n",
+ "R_1 = 1 #p - The force applied at b\n",
+ "R_2 = 1 #p - The force applied at c\n",
+ "l_ab = 1 #L\n",
+ "l_bc = 1 #L \n",
+ "\n",
+ "#Logical step \n",
+ "#Since the system is in symmetry we can avoid moment M = 0 caliculations\n",
+ "\n",
+ "#F_Y = 0 \n",
+ "R_A = (R_1 + R_2)/2\n",
+ "R_B = (R_1 + R_2)/2\n",
+ "\n",
+ "#Lets take '3' sections \n",
+ "#Considering section 1-----1 at 0.5L\n",
+ "l_1 = 0.5 #L - distance of the section from the A\n",
+ "v_1 = R_A #F_Y = 0 \n",
+ "M_1 = R_A*l_1 #MAking moment at section 1 = 0\n",
+ "\n",
+ "#Considering section 2-----2 at 1L\n",
+ "l_2 = 1 #L - distance of the section from the A\n",
+ "v_2 = R_A #F_Y = 0 \n",
+ "M_2 = R_A*l_2 #MAking moment at section 2 = 0\n",
+ "\n",
+ "#Considering section 3-----3 at 1.5L\n",
+ "l_3 = 1.5 #L - distance of the section from the A\n",
+ "v_3 = 0 #F_Y = 0 \n",
+ "M_3 = R_A*l_2 #MAking moment at section 2 = 0 and symmetry \n",
+ "\n",
+ "#GRAPH\n",
+ "#Since the symmetry exists the graphs are also symmetry\n",
+ "%matplotlib inline\n",
+ "import math \n",
+ "from matplotlib.pyplot import plot,suptitle,xlabel,ylabel\n",
+ "#Drawing of shear and bending moment diagram\n",
+ "print \"Given problem is for drawing diagram, this diagram is drawn by step by step manner. \"\n",
+ "X = [0,0.5,1,1.000000001,1.5,1.999999999999,2,2.5,3] # For graph precision \n",
+ "\n",
+ "V = [R_A,v_1,v_2,v_3,v_3,v_3,-v_2,-v_1,-R_B];\t\t\t#Shear matrix\n",
+ "M = [0,M_1,M_2,1,1,1,M_2,M_1,0];\t\t\t#Bending moment matrix\n",
+ "plot(X,V);\t\t\t#Shear diagram\n",
+ "plot(X,M);\t\t\t#Bending moment diagram\n",
+ "suptitle( 'Shear and bending moment diagram')\n",
+ "xlabel('X axis')\n",
+ "ylabel( 'Y axis') ;"
+ ],
+ "language": "python",
+ "metadata": {},
+ "outputs": [
+ {
+ "output_type": "stream",
+ "stream": "stdout",
+ "text": [
+ "Given problem is for drawing diagram, this diagram is drawn by step by step manner. \n"
+ ]
+ },
+ {
+ "metadata": {},
+ "output_type": "display_data",
+ "png": 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+ "text": [
+ "<matplotlib.figure.Figure at 0x8154240>"
+ ]
+ }
+ ],
+ "prompt_number": 127
+ },
+ {
+ "cell_type": "heading",
+ "level": 2,
+ "metadata": {},
+ "source": [
+ "Example 5.8 page nmber 244"
+ ]
+ },
+ {
+ "cell_type": "code",
+ "collapsed": false,
+ "input": [
+ "#Given \n",
+ "l_ab = 1.0 #L - The length of the beam\n",
+ "F_D = 1.0 #W - The force distribution \n",
+ "F = F_D*l_ab #WL - The force applied\n",
+ "#Beause of symmetry the moment caliculations can be neglected\n",
+ "#F_Y = 0\n",
+ "R_A = F/2 #wl - The reactive force at A\n",
+ "R_B = F/2 #wl - The reactive force at B\n",
+ "\n",
+ "#considering many sections \n",
+ "\n",
+ "#section 1--1\n",
+ "l_1 = [0,0.1,0.2,0.3,0.4,0.5,0.6,0.7,0.8,0.9,1] #L taking each section at 0.1L distance \n",
+ "M_1 = [0,0,0,0,0,0,0,0,0,0,0]\n",
+ "v = [0,0,0,0,0,0,0,0,0,0,0]\n",
+ "for i in range(10):\n",
+ " v[i] = R_A - F_D*l_1[i] \n",
+ " M_1[i] = R_A*l_1[i] - F_D*(l_1[i]**2)/2 #M = 0 in the section\n",
+ "print R_A\n",
+ "#Graphs\n",
+ "import numpy as np\n",
+ "values = [0.5,0,-0.5]\n",
+ "y = np.array(values)\n",
+ "t = np.linspace(0,1,3)\n",
+ "poly_coeff = np.polyfit(t, y, 2)\n",
+ "import matplotlib.pyplot as plt\n",
+ "plt.plot(t, y, 'o')\n",
+ "plt.plot(t, np.poly1d(poly_coeff)(t), '-')\n",
+ "plt.show()\n",
+ "\n",
+ "import numpy as np\n",
+ "values = M_1\n",
+ "y = np.array(values)\n",
+ "t = np.linspace(0,1,11)\n",
+ "poly_coeff = np.polyfit(t, y, 2)\n",
+ "import matplotlib.pyplot as plt\n",
+ "plt.plot(t, y, 'o')\n",
+ "plt.plot(t, np.poly1d(poly_coeff)(t), '-')\n",
+ "plt.show()"
+ ],
+ "language": "python",
+ "metadata": {},
+ "outputs": [
+ {
+ "output_type": "stream",
+ "stream": "stdout",
+ "text": [
+ "0.5\n"
+ ]
+ },
+ {
+ "metadata": {},
+ "output_type": "display_data",
+ "png": 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+ "text": [
+ "<matplotlib.figure.Figure at 0x87884e0>"
+ ]
+ },
+ {
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R6pNEAAAAAElFTkSuQmCC\n",
+ "text": [
+ "<matplotlib.figure.Figure at 0x9e8f588>"
+ ]
+ }
+ ],
+ "prompt_number": 111
+ },
+ {
+ "cell_type": "heading",
+ "level": 2,
+ "metadata": {},
+ "source": [
+ "Example 5.9 page number 245"
+ ]
+ },
+ {
+ "cell_type": "code",
+ "collapsed": false,
+ "input": [
+ "#Given \n",
+ "P_Max = 10 #N - the maximum distribution in a triangular distribution\n",
+ "L = 3 #mt the total length of force distribution \n",
+ "L_X = 5 #mt - the horizantal length of the rod\n",
+ "#caliculations \n",
+ "\n",
+ "F_y = P_Max*L*0.5 #N - The force due to triangular distribition \n",
+ "L_com = 2*L /3 #mt - the resultant force acting as a result of distribution acting position \n",
+ "#F_X = 0 forces in x directions\n",
+ "R_A_X = 0 # since there are no forces in X-direction\n",
+ "R_B_X = 0\n",
+ "#M_A = 0 momentum at point a is zero\n",
+ "#F_y*L_com - R_B_Y*L_X = 0\n",
+ "R_B_Y = F_y*L_com/L_X\n",
+ "\n",
+ "#M_B= 0 momentum at point b is zero\n",
+ "#- R_A_Y*L_X = F_y*(L_X-L )\n",
+ "\n",
+ "R_A_Y = - F_y*L/L_X\n",
+ "\n",
+ "#caliculating for some random value\n",
+ "#For a---a section \n",
+ "l_a = 2 #mt - a---a section from a \n",
+ "l_com_a = 2*l_a/3\n",
+ "v_a = R_A_Y + 0.5*l_a*(10.0*2/3) #*(10*2/3) because the maximum moves\n",
+ "\n",
+ "M_a = (10.0*0.66)*l_a*(0.33) + R_A_Y*l_a\n",
+ "\n",
+ "print \"The force and moment in section a--a are\",round(v_a,2),\"KN ,\",M_a,\"KN-m\"\n",
+ "\n"
+ ],
+ "language": "python",
+ "metadata": {},
+ "outputs": [
+ {
+ "output_type": "stream",
+ "stream": "stdout",
+ "text": [
+ "The force and moment in section a--a are -2.33 KN , -13.644 KN-m\n"
+ ]
+ }
+ ],
+ "prompt_number": 112
+ },
+ {
+ "cell_type": "heading",
+ "level": 2,
+ "metadata": {},
+ "source": [
+ "Example 5.13 page number 254"
+ ]
+ },
+ {
+ "cell_type": "code",
+ "collapsed": false,
+ "input": [
+ "#Given\n",
+ "l_ab = 4 #L - The total length lets say '3L'\n",
+ "R_1 = 1 #p - The force applied at b\n",
+ "R_2 = 1 #p - The force applied at c\n",
+ "l_ab = 1 #L\n",
+ "l_bc = 3 #L \n",
+ "\n",
+ "#Logical step \n",
+ "#Since the system is in symmetry we can avoid moment M = 0 caliculations\n",
+ "\n",
+ "#F_Y = 0 \n",
+ "R_A = (R_1 + R_2)/2\n",
+ "R_B = (R_1 + R_2)/2\n",
+ "\n",
+ "#Lets take '3' sections \n",
+ "#Considering section 1-----1 at 0.5L\n",
+ "l_1 = 0.5 #L - distance of the section from the A\n",
+ "v_1 = R_A #F_Y = 0 \n",
+ "M_1 = R_A*l_1 #MAking moment at section 1 = 0\n",
+ "\n",
+ "#Considering section 2-----2 at 1L\n",
+ "l_2 = 1 #L - distance of the section from the A\n",
+ "v_2 = R_A #F_Y = 0 \n",
+ "M_2 = R_A*l_2 #MAking moment at section 2 = 0\n",
+ "\n",
+ "#Considering section 3-----3 at 1.5L\n",
+ "l_3 = 3 #L - distance of the section from the A\n",
+ "v_3 = 0 #F_Y = 0 \n",
+ "M_3 = R_A*l_2 #MAking moment at section 2 = 0 and symmetry \n",
+ "\n",
+ "#GRAPH\n",
+ "#Since the symmetry exists the graphs are also symmetry\n",
+ "%matplotlib inline\n",
+ "import math \n",
+ "from matplotlib.pyplot import plot,suptitle,xlabel,ylabel\n",
+ "#Drawing of shear and bending moment diagram\n",
+ "print \"Given problem is for drawing diagram, this diagram is drawn by step by step manner. \"\n",
+ "X = [0,0.5,1,1.0000001,2,2.9999999999,3,3.5,4] # For graph precision \n",
+ "\n",
+ "V = [R_A,v_1,v_2,v_3,v_3,v_3,-v_2,-v_1,-R_B];\t\t\t#Shear matrix\n",
+ "M = [0,M_1,M_2,M_3,M_3,M_3,M_2,M_1,0];\t\t\t#Bending moment matrix\n",
+ "plot(X,V);\t\t\t#Shear diagram\n",
+ "plot(X,M);\t\t\t#Bending moment diagram\n",
+ "suptitle( 'Shear and bending moment diagram')\n",
+ "xlabel('X axis')\n",
+ "ylabel( 'Y axis') ;"
+ ],
+ "language": "python",
+ "metadata": {},
+ "outputs": [
+ {
+ "output_type": "stream",
+ "stream": "stdout",
+ "text": [
+ "Given problem is for drawing diagram, this diagram is drawn by step by step manner. \n"
+ ]
+ },
+ {
+ "metadata": {},
+ "output_type": "display_data",
+ "png": 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VtAAAAABJRU5ErkJggg==\n",
+ "text": [
+ "<matplotlib.figure.Figure at 0x9e8f1d0>"
+ ]
+ }
+ ],
+ "prompt_number": 126
+ },
+ {
+ "cell_type": "heading",
+ "level": 2,
+ "metadata": {},
+ "source": [
+ "Example 5.14 page number 255"
+ ]
+ },
+ {
+ "cell_type": "code",
+ "collapsed": false,
+ "input": [
+ "#Given\n",
+ "l = 1.0 #l - The length of the beam\n",
+ "p = 1.0 #W - The total load applied\n",
+ "#since it is triangular distribution \n",
+ "l_com = 0.66*l#l - The distance of force of action from one end\n",
+ "#F_Y = 0\n",
+ "#R_A + R_B = p\n",
+ "#M_a = 0 Implies that R_B = 2*R_A\n",
+ "R_A = p/3.0\n",
+ "R_B = 2.0*p/3\n",
+ "\n",
+ "#Taking Many sections \n",
+ "\n",
+ "#Section 1----1\n",
+ "l = [0,0.1,0.2,0.3,0.4,0.5,0.6,0.7,0.8,0.9,1] #L taking each section at 0.1L distance \n",
+ "M = [0,0,0,0,0,0,0,0,0,0,0]\n",
+ "v = [0,0,0,0,0,0,0,0,0,0,0]\n",
+ "for i in range(10):\n",
+ " v[i] = p*(l[i]**2) - p/3.0\n",
+ " M[i] = p*(l[i]**3)/(3.0)- p*l[i]/3.0\n",
+ "\n",
+ "v[10] = R_B #again concluded Because the value is tearing of \n",
+ "\n",
+ "\n",
+ "#Graph\n",
+ "import numpy as np\n",
+ "values = M\n",
+ "y = np.array(values)\n",
+ "t = np.linspace(0,1,11)\n",
+ "poly_coeff = np.polyfit(t, y, 2)\n",
+ "import matplotlib.pyplot as plt\n",
+ "plt.plot(t, y, 'o')\n",
+ "plt.plot(t, np.poly1d(poly_coeff)(t), '-')\n",
+ "plt.show()\n",
+ "import numpy as np\n",
+ "values = v\n",
+ "y = np.array(values)\n",
+ "t = np.linspace(0,1,11)\n",
+ "poly_coeff = np.polyfit(t, y, 2)\n",
+ "import matplotlib.pyplot as plt\n",
+ "plt.plot(t, y, 'o')\n",
+ "plt.plot(t, np.poly1d(poly_coeff)(t), '-')\n",
+ "plt.show()\n",
+ "\n",
+ "\n",
+ "\n",
+ "\n"
+ ],
+ "language": "python",
+ "metadata": {},
+ "outputs": [
+ {
+ "metadata": {},
+ "output_type": "display_data",
+ "png": 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+ "text": [
+ "<matplotlib.figure.Figure at 0x80c3f98>"
+ ]
+ },
+ {
+ "metadata": {},
+ "output_type": "display_data",
+ "png": 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ZdY50jZFysGNhZteXHYPFZvaxmZ0ZRJ11rTq/E2XtuphZkZn1j2R9kVTN70dK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\nbKRBM81FAAAAAElFTkSuQmCC\n",
+ "text": [
+ "<matplotlib.figure.Figure at 0xa487c18>"
+ ]
+ }
+ ],
+ "prompt_number": 5
+ },
+ {
+ "cell_type": "heading",
+ "level": 2,
+ "metadata": {},
+ "source": [
+ "Example 5.16 page number 259"
+ ]
+ },
+ {
+ "cell_type": "code",
+ "collapsed": false,
+ "input": [
+ "#Given\n",
+ "l = 6.0 #a - length of the rod\n",
+ "F = 1.0 #p - force applies in x direction \n",
+ "d = 1.0 #a \n",
+ "M = 1.0 #pa - torque applies on the rod\n",
+ "l_ab = 4.0 #a application of torque point from A\n",
+ "#M = 0 implies that\n",
+ "R_A = F/6.0 #p - The reaction at A\n",
+ "R_B = - R_A #F_Y = 0\n",
+ "\n",
+ "#Caliculations \n",
+ "\n",
+ "#Taking sections \n",
+ "#Section 1---1\n",
+ "l_1 = 1 #a - the length of the section \n",
+ "M_1 = - R_A*l_1 #M = 0\n",
+ "\n",
+ "#Section 2---2\n",
+ "l_2 = 4 #a - the length of the section \n",
+ "M_2 = - R_A*l_2 #M = 0\n",
+ "\n",
+ "l_4 = 2 #a - the length of the section \n",
+ "M_4 = 1/3.0 #pa #M = 0 '-M' because there is moment couple in between\n",
+ "\n",
+ "\n",
+ "#Section 3---3\n",
+ "l_3 = 1 #a - the length of the section \n",
+ "M_3 = 1/6.0#pa M = 0 '-M' because there is moment couple in between\n",
+ "print R_A\n",
+ "\n",
+ "#GRAPH\n",
+ "#Since the symmetry exists the graphs are also symmetry\n",
+ "%matplotlib inline\n",
+ "import math \n",
+ "from matplotlib.pyplot import plot,suptitle,xlabel,ylabel\n",
+ "#Drawing of shear and bending moment diagram\n",
+ "print \"Given problem is for drawing diagram, this diagram is drawn by step by step manner. \"\n",
+ "X = [0,1,4,4.00001,5,6] # For graph precision \n",
+ "M = [0,M_1,M_2,M_4,M_3,0];\t\t\t#Bending moment matrix\n",
+ "plot(X,M);\t\t\t#Bending moment diagram\n",
+ "suptitle( 'Shear and bending moment diagram')\n",
+ "xlabel('X axis')\n",
+ "ylabel( 'Y axis') ;\n",
+ "\n",
+ "\n",
+ "\n",
+ "\n",
+ "\n",
+ "\n",
+ "\n",
+ "\n"
+ ],
+ "language": "python",
+ "metadata": {},
+ "outputs": [
+ {
+ "output_type": "stream",
+ "stream": "stdout",
+ "text": [
+ "0.166666666667\n",
+ "Given problem is for drawing diagram, this diagram is drawn by step by step manner. \n"
+ ]
+ },
+ {
+ "metadata": {},
+ "output_type": "display_data",
+ "png": 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+ "text": [
+ "<matplotlib.figure.Figure at 0x9e65940>"
+ ]
+ }
+ ],
+ "prompt_number": 150
+ },
+ {
+ "cell_type": "code",
+ "collapsed": false,
+ "input": [],
+ "language": "python",
+ "metadata": {},
+ "outputs": []
+ }
+ ],
+ "metadata": {}
+ }
+ ]
+}
\ No newline at end of file |