{ "metadata": { "name": "", "signature": "sha256:be59baaa0b424ca36821aba74f7944f301ffd891c617783ec6544d131134dbbb" }, "nbformat": 3, "nbformat_minor": 0, "worksheets": [ { "cells": [ { "cell_type": "heading", "level": 1, "metadata": {}, "source": [ "Chapter 10 : The Boundary Layer" ] }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example 10.1 Page No : 379" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "\t\t\t\n", "#Initialization of variables\n", "v = 30. \t\t\t#velocity - m/s\n", "nu = 1.5e-5 \t\t\t#m**2/s\n", "\t\t\t\n", "#calculations\n", "Re = 5*10**5\n", "xc = Re*nu/v\n", "\t\t\t\n", "#results\n", "print \"Transistion region = %.2f m\"%(xc)" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Transistion region = 0.25 m\n" ] } ], "prompt_number": 1 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example 10.2 Page No : 388" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "\t\t\t\n", "#Initialization of variables\n", "u = 2. \t\t\t #velocity - m/s\n", "x = 0.15 \t\t\t#length - m\n", "nu = 1.5e-5 \t\t#m**2/s\n", "B = 0.5 \t\t\t#m\n", "rho = 1.22 \t\t\t#kg/m**3\n", "\n", "#calcualtions\n", "Rx = u*x/nu\n", "delta = 4.91*x/math.sqrt(Rx)\n", "deltas = 1.729*x/math.sqrt(Rx)\n", "Cf = 1.328/math.sqrt(Rx)\n", "Ff = Cf*0.5*rho*u**2 *2*B*x\n", "\t\t\t\n", "#results\n", "print \"Boundary layer thickness = %.2f cm\"%(delta*100)\n", "print \" Displacement thickness = %.2f cm\"%(deltas*100)\n", "print \" Average drag coeffcient = %.4f\"%(Cf)\n", "print \" Drag force = %.4f N\"%(Ff)" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Boundary layer thickness = 0.52 cm\n", " Displacement thickness = 0.18 cm\n", " Average drag coeffcient = 0.0094\n", " Drag force = 0.0034 N\n" ] } ], "prompt_number": 2 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example 10.5 Page No : 400" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "\t\t\t\n", "#Initialization of variables\n", "U = 172.*1000/3600 \t\t\t#m/s\n", "w = 3. \t \t\t#m\n", "h = 3. \t\t \t#m\n", "L = 100. \t\t\t #m\n", "nu = 1.5e-5 \t\t\t#m**2/s\n", "rho = 1.22 \t \t\t#kg/m**3\n", "\t\t\t\n", "#calculations\n", "Rl = U*L/nu\n", "Cf = 0.074 /(Rl**(1./5))\n", "Ff = Cf*0.5*rho*U**2 *w*h*L\n", "power = Ff*U\n", "\t\t\t\n", "#results\n", "print \"power required = %.1f kW\"%(power/1000)\n", "#The answer is a bit different due to rounding off error" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "power required = 88.3 kW\n" ] } ], "prompt_number": 3 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example 10.6 Page No : 400" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math \n", "\t\t\t\n", "#Initialization of variables\n", "U = 4000. \t\t \t#m/s\n", "L = 8. \t\t \t#m\n", "nu = 3600.e-6 \t\t\t#m**2/s\n", "rho = 1000. \t\t\t#kg/m**3\n", "b = 5. \t\t\t#m\n", "\t\t\t\n", "#calculations\n", "Rl = U*L/nu\n", "Cf = 0.074/Rl**(1./5) -1700/Rl\n", "Ff = Cf*0.5*rho*(U/3600)**2 *L*b\n", "\t\t\t\n", "#results\n", "print \"Skin friction drag = %.2f N\"%(Ff)\n", "\n", "# note : rounding off error." ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Skin friction drag = 69.75 N\n" ] } ], "prompt_number": 1 } ], "metadata": {} } ] }