{ "metadata": { "name": "" }, "nbformat": 3, "nbformat_minor": 0, "worksheets": [ { "cells": [ { "cell_type": "heading", "level": 1, "metadata": {}, "source": [ "Chapter 9 : Agitation" ] }, { "cell_type": "heading", "level": 3, "metadata": {}, "source": [ "Example 9.3 - Page No :389\n" ] }, { "cell_type": "code", "collapsed": false, "input": [ "\n", "import math\n", "\n", "# Variables\n", "Nblades = 4.; \t\t\t # no. of blades\n", "d = 9/12.; \t\t\t #[ft] - diameter of the impeller\n", "dt = 30/12.; \t\t\t #[ft] - diameter of the math.tank\n", "Nbaffles = 4. \t\t\t # no. of baffles\n", "h = 30.; \t \t\t # [inch] - height of unit\n", "mu = 10.; \t\t\t #[cP] - vismath.cosity of fluid_\n", "sg = 1.1; \t\t \t # specific gravity of fluid_\n", "s = 300. \t\t\t #[rpm] - speed of agitator\n", "CbyT = 0.3; \n", "\n", "# Calculations\n", "V = (math.pi*dt**3)/4; \t #volume of math.tank in ft**3\n", "V1 = V*7.48; \t\t\t #[gal] - volume of math.tank in gallons\n", "mu = mu*(6.72*10**-4); #[lb/ft*sec]\n", "p = sg*62.4; \t\t\t #[lb/ft**3] - density of fluid_\n", "N = s/60.; \t\t\t #[rps] - impeller speed in revolutions per second\n", "Nre = ((d**2)*N*p)/mu;\n", "\n", "# Results\n", "print \"Nre = %.2e\"%Nre\n", "print \" Therefore the agitator operates in the turbulent region\"\n", "Npo = 1.62;\n", "gc = 32.174;\n", "P = (Npo*(p*(N**3)*(d**5)))/(gc*550);\n", "Cf = 63025.;\n", "Tq = (P/s)*Cf;\n", "PbyV = P/V;\n", "PbyV1 = P/V1;\n", "TqbyV = Tq/V;\n", "TqbyV1 = Tq/V1;\n", "print \" The power per unit volume and the torque per unit volume is \\nP/V = %.2ef hp/ft**3 = %.2e \\\n", "hp/gal \\nTq/V = %.2f in*lb/ft**3 = %.3f in*lb/gal\"%(PbyV,PbyV1,TqbyV,TqbyV1);" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Nre = 2.87e+04\n", " Therefore the agitator operates in the turbulent region\n", " The power per unit volume and the torque per unit volume is \n", "P/V = 1.52e-02f hp/ft**3 = 2.03e-03 hp/gal \n", "Tq/V = 3.19 in*lb/ft**3 = 0.427 in*lb/gal\n" ] } ], "prompt_number": 6 }, { "cell_type": "heading", "level": 3, "metadata": {}, "source": [ "Example 9.4 - Page No :391\n" ] }, { "cell_type": "code", "collapsed": false, "input": [ "\n", "# Variables\n", "Tpilot = 30.;\n", "Tlab = 10.;\n", "N1 = 690.;\n", "N2 = 271.;\n", "D2 = 3.;\n", "D1 = 1.;\n", "\n", "# Calculations\n", "n = (math.log(N1/N2))/(math.log(D2/D1));\n", "V = 12000/7.48; \t\t\t #[ft**3]\n", "T = ((4.*V)/math.pi)**(1./3); \t\t\t #[ft]\n", "R = 12.69/(30/12.);\n", "N3 = N2*(1./R)**n; \t\t\t #[rpm] - impeller speed in the reactor\n", "\n", "# Results\n", "print \"impeller speed in rpm = %f\"%round(N3,4)\n", "D3 = 0.75*R; \t\t\t #[ft] - reactor impeller diameter\n", "print \"reactor impeller diameter in ft = %.3f\"%D3\n", "P = 0.1374*((N3/N2)**3)*(R**5);\n", "print \"power in hp = %.3f\"%P\n", "Cf = 63025.;\n", "Tq = (P/N3)*Cf; \t\t\t #[inch*lb]\n", "print \"torque in inch*lb = %.0f\"%Tq\n", "print \"At this point, the design is complete. \\nA sarc ard size impeller would be chosen as \\\n", " well as a tan ard size motor7.5 hp or 10 hp\"\n", "\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "impeller speed in rpm = 68.044500\n", "reactor impeller diameter in ft = 3.807\n", "power in hp = 7.329\n", "torque in inch*lb = 6789\n", "At this point, the design is complete. \n", "A sarc ard size impeller would be chosen as well as a tan ard size motor7.5 hp or 10 hp\n" ] } ], "prompt_number": 19 }, { "cell_type": "heading", "level": 3, "metadata": {}, "source": [ "Example 9.5 - Page No : 393\n" ] }, { "cell_type": "code", "collapsed": false, "input": [ "\n", "\n", "from numpy import *\n", "\n", "\n", "# Variables\n", "# given\n", "n = array([0.5, 0.6, 0.7, 0.8, 0.9, 1.0]);\n", "D2 = 3.806;\n", "D1 = 0.25;\n", "R = D2/D1;\n", "N1 = 690.;\n", "\n", "# Calculations\n", "N2 = N1*((D1/D2)**n);\n", "P1 = 9.33*10**-3; \t\t\t #[hp]\n", "P2 = P1*R**(5.-3*n);\n", "\n", "# Results\n", "print \" n N,rpm P,hp\"\n", "for i in range(6):\n", " print \" %f %4.0f %4.0f\"%(n[i],N2[i],P2[i]);\n", "\n", "\n", "# Answers may be differ because of rounding error." ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ " n N,rpm P,hp\n", " 0.500000 177 128\n", " 0.600000 135 57\n", " 0.700000 103 25\n", " 0.800000 78 11\n", " 0.900000 60 5\n", " 1.000000 45 2\n" ] } ], "prompt_number": 29 } ], "metadata": {} } ] }