{ "metadata": { "name": "", "signature": "sha256:e9347bdc41c6b4bda65f9d26d446767053e6f25c72d5803a3f6994404d86363c" }, "nbformat": 3, "nbformat_minor": 0, "worksheets": [ { "cells": [ { "cell_type": "heading", "level": 1, "metadata": {}, "source": [ "Chapter 8 : Impact of Jets" ] }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example 8.1 Page No : 276" ] }, { "cell_type": "code", "collapsed": false, "input": [ "\n", "import math \n", "\t\t\n", "#initialisation of variables\n", "d = 1. \t\t#in\n", "v = 36. \t\t#ft/sec\n", "b = 30. \t\t#degrees\n", "w = 62.4 \t\t#lbs/ft**3\n", "g = 32.2\n", "\t\t\n", "#CALCULATIONS\n", "a = math.pi/4 * (d/12)**2\n", "thrust = w*a*v**2/g\n", "P = w* math.sin(math.radians(b))*v**2*(math.pi*(d/12)**2/4)/g\n", "\t\t\n", "#RESULTS\n", "print \"The trust when the plate is normal to the jet = %.1f lbs. wt.\"%thrust\n", "print 'Total thrust on the plate when inclined = %.2f lb wt'%(P)\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "The trust when the plate is normal to the jet = 13.7 lbs. wt.\n", "Total thrust on the plate when inclined = 6.85 lb wt\n" ] } ], "prompt_number": 1 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example 8.2 Page No : 277" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "\t\t\n", "#initialisation of variables\n", "a = 180. \t\t#degrees\n", "g = 32.2 \t\t#ft/sec**2\n", "w = 62.4 \t\t#lbs/ft**3\n", "d = 1. \t\t#in\n", "H = 100. \t\t#ft\n", "u = 0.95\n", "\t\t\n", "#CALCULATIONS\n", "v = u*math.sqrt(2*g*H)\n", "Px = w*(1- math.cos(math.radians(a)))*(math.pi*(d/12)**2/4)*v**2/g\n", "\t\t\n", "#RESULTS\n", "print 'force it exerts = %.1f lb wt'%(Px)\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "force it exerts = 122.9 lb wt\n" ] } ], "prompt_number": 2 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example 8.3 Page No : 278" ] }, { "cell_type": "code", "collapsed": false, "input": [ "\n", "import math \n", "\t\t\n", "#initialisation of variables\n", "d = 30. \t\t#in\n", "a = 90. \t\t#degrees\n", "Q = 62.5 \t\t#ft**3/sec\n", "w = 62.4 \t\t#lbs/ft**3\n", "n =4.\n", "g =32.2\n", "\t\t\n", "#CALCULATIONS\n", "v = Q*4/(math.pi*(d/12)**2)\n", "P = w*math.pi*(d/12)**2*v**2/(4*g)\n", "Px = P/n\n", "\n", "#RESULTS\n", "print 'pull on each bolt = %.1f lbs'%(Px)\n", "\n", "# rounding off error. please check." ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "pull on each bolt = 385.5 lbs\n" ] } ], "prompt_number": 2 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example 8.4 Page No : 278" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "\t\t\n", "#initialisation of variables\n", "d = 4. \t\t#in\n", "v = 30. \t\t#ft/sec\n", "a = 22.5 \t\t#degrees\n", "w = 62.4 \t\t#lbs/ft**3\n", "g = 32.2 \t\t#ft/sec**2\n", "\t\t\n", "#CALCULATIONS \n", "P = w*(math.pi*(d/12)**2/4)*v**2*math.sqrt(2*(1-math.cos(math.radians(a))))/g\n", "\t\t\n", "#RESULTS\n", "print 'Resultant force tending to move the pipe = %.f lbs'%(P)\n", "\n", "\n", "\t\t#ANSWER GIVEN IN THE TEXTBOOK IS WRONG\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Resultant force tending to move the pipe = 59 lbs\n" ] } ], "prompt_number": 4 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example 8.5 Page No : 284" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "\t\t\n", "#initialisation of variables\n", "d = 3. \t\t#in\n", "v1 = 80. \t\t#ft/sec\n", "v2 = 40. \t\t#ft/sec\n", "w = 62.4 \t\t#lbs/ft**3\n", "g = 32.2 \t\t#ft/sec**2\n", "\t\t\n", "#CALCULATIONS\n", "vr = v1-v2\n", "P = w*vr*v2*math.pi*(d/12)**2/(g*4)\n", "\t\t\n", "#RESULTS\n", "print 'normal pressure on the plate when jet strikes = %.1f lbs'%(P)\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "normal pressure on the plate when jet strikes = 152.2 lbs\n" ] } ], "prompt_number": 5 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example 8.6 Page No : 285" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "\t\t\n", "#initialisation of variables\n", "d = 2. \t\t#in\n", "v1 = 50. \t\t#ft/sec\n", "v2 = 20. \t\t#ft/sec\n", "W = 62.4 \t\t#lbs/ft**3\n", "g = 32.2 \t\t#ft/sec**2\n", "\t\t\n", "#CALCULATIONS\n", "vr = v1-v2\n", "P = W*vr*v1*math.pi*(d/2)**2/(g*4)\n", "W = P*v2\n", "KE = 2*vr*v2*100/v1**2\n", "\t\t\n", "#RESULTS\n", "print 'Efficiency = %.f per cent'%(KE)\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Efficiency = 48 per cent\n" ] } ], "prompt_number": 6 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example 8.7 Page No : 286" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "\n", "#initialisation of variables\n", "d = 1. \t\t#in\n", "v = 10. \t\t#f/sec\n", "v1 = 30. \t\t#ft/sec\n", "w = 62.4 \t\t#lbs/ft**3\n", "a = 180. \t\t#degrees\n", "g = 32.2 \t\t#ft/sec**2\n", "\t\t\n", "#CALCULATIONS\n", "A = math.pi*(d/12)**2/4\n", "vr = 80-v1\n", "M = w*vr*A\n", "Px = M*vr*(1- math.cos(math.radians(a)))/g\n", "W = Px*v1\n", "M1 = w*80*A\n", "Px1 = M1*vr*(1-math.cos(math.radians(a)))/g\n", "W1 = Px1*v1\n", "\t\t\n", "#RESULTS\n", "print 'total force when there is a math.single cup = %.1f ft lbs'%(W)\n", "print ' total force when there is a series of cups = %.1f ft lbs'%(W1)\n", "\n", "# rounding off error." ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "total force when there is a math.single cup = 1585.4 ft lbs\n", " total force when there is a series of cups = 2536.7 ft lbs\n" ] } ], "prompt_number": 3 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example 8.8 Page No : 287" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "\t\t\n", "#initialisation of variables\n", "v = 100. \t\t#ft/sec\n", "u = 40. \t\t#ft/sec\n", "a = 25. \t\t#degrees\n", "g = 32.2 \t\t#ft/sec**2\n", "vr = 66. \t\t#ft/sec\n", "a1 = 20. \t\t#/degrees\n", "a2 = 8. \t\t#degrees\n", "r = 0.14\n", "\t\t\n", "#CALCULATIONS\n", "Uw = v * math.cos(math.radians(a))\n", "Uv = v * math.sin(math.radians(a))\n", "tanA = Uv/(Uw - u)\n", "A = math.degrees(math.atan(tanA))\n", "v1 = vr*.14/0.342\n", "W = (v**2-v1**2)/(2*g)\n", "e = (v**2-v1**2)*100/v**2\n", "\n", "#RESULTS\n", "print 'inlet blade angle = %.2f degrees'%(A)\n", "print ' Work done = %.f ft lbs'%(W)\n", "print ' efficiency = %.2f ft per cent'%(e)\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "inlet blade angle = 39.85 degrees\n", " Work done = 144 ft lbs\n", " efficiency = 92.70 ft per cent\n" ] } ], "prompt_number": 19 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example 8.9 Page No : 291" ] }, { "cell_type": "code", "collapsed": false, "input": [ "\t\t\n", "#initialisation of variables\n", "Q = 60. \t\t#ft**3/sec\n", "v = 12. \t\t#m.p.h\n", "A = 3. \t\t#ft**2\n", "D = 64. \t\t#lbs/ft**3\n", "g = 32.2 \t\t#ft/sec**2\n", "M = 64. \t\t#lbs\n", "\t\t\n", "#CALCULATIONS\n", "vr = Q/A\n", "u = v*44/30\n", "v1 = vr-u\n", "P = M*Q*v1/g\n", "\t\t\n", "#RESULTS\n", "print 'propelling force = %.1f lbs'%(P)\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "propelling force = 286.2 lbs\n" ] } ], "prompt_number": 10 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example 8.10 Page No : 291" ] }, { "cell_type": "code", "collapsed": false, "input": [ "\t\t\n", "#initialisation of variables\n", "vr = 20. \t\t#f/sec\n", "u = 9. \t\t#knots\n", "D = 64. \t\t#lbs per cubic foot\n", "g = 32.2 \t\t#ft/sec**2\n", "p = 40. \t\t#per cent\n", "\t\t\n", "#CALCULATIONS\n", "u1 = u*6080/3600\n", "v = vr-u1\n", "P = D*2*vr*4.8/g\n", "HP = P*u1/550\n", "HP1 = 100*HP/p\n", "\t\t\n", "#RESULTS\n", "print 'cylinder H.P = %.2f H.P'%(HP1)\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "cylinder H.P = 26.37 H.P\n" ] } ], "prompt_number": 11 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example 8.11 Page No : 293" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "\t\t\n", "#initialisation of variables\n", "W = 62.4 \t\t#lbs/ft**3\n", "A = 4. \t \t#ft**2\n", "P = 1000. \t\t#lbs\n", "g = 32.2 \t\t#ft/sec**2\n", "v = 10. \t\t#ft/sec\n", "\t\t\n", "#CALCULATIONS\n", "vr = math.sqrt(25+(P*g/(W*A)))+5\n", "Q = vr*W*A/10\n", "e = 2*v*100/(vr+v)\n", "\t\t\n", "#RESULTS\n", "print 'quantity of water pumped = %.1f lbs'%(Q)\n", "print ' efficiency = %.1f per cent'%(e)\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "quantity of water pumped = 434.6 lbs\n", " efficiency = 73.0 per cent\n" ] } ], "prompt_number": 12 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example 8.12 Page No : 294" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "\t\t\n", "#initialisation of variables\n", "g = 32.2 \t\t#ft/sec**2\n", "\t\t\n", "#CALCULATIONS\n", "v = math.sqrt(32*g)\n", "\t\t\n", "#RESULTS\n", "print 'speed that delivery commence = %.1f ft/sec'%(v)\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "speed that delivery commence = 32.1 ft/sec\n" ] } ], "prompt_number": 13 } ], "metadata": {} } ] }