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Diffstat (limited to 'Aircraft_Structures_for_Engineering_Students/Chapter09.ipynb')
-rwxr-xr-x | Aircraft_Structures_for_Engineering_Students/Chapter09.ipynb | 97 |
1 files changed, 0 insertions, 97 deletions
diff --git a/Aircraft_Structures_for_Engineering_Students/Chapter09.ipynb b/Aircraft_Structures_for_Engineering_Students/Chapter09.ipynb deleted file mode 100755 index 119bd5b2..00000000 --- a/Aircraft_Structures_for_Engineering_Students/Chapter09.ipynb +++ /dev/null @@ -1,97 +0,0 @@ -{
- "metadata": {
- "name": "",
- "signature": "sha256:47a0669d4632eab71f162a005cd6d69531f951e47ad9f34d928b679209ff2467"
- },
- "nbformat": 3,
- "nbformat_minor": 0,
- "worksheets": [
- {
- "cells": [
- {
- "cell_type": "heading",
- "level": 1,
- "metadata": {},
- "source": [
- "Chapter 09: Thin plates"
- ]
- },
- {
- "cell_type": "heading",
- "level": 2,
- "metadata": {},
- "source": [
- "Example 9.1 Pg.No.310"
- ]
- },
- {
- "cell_type": "code",
- "collapsed": false,
- "input": [
- "from __future__ import division\n",
- "import math\n",
- "\n",
- "h=400 #height of structure (mm)\n",
- "l1=300 #length of small section (mm)\n",
- "L=1200 #length of whole structure (mm)\n",
- "E=70000 #youngs modulus (N/mm^2)\n",
- "A_f=350 #area of flange (mm^2)\n",
- "A_s=300 # area of stiffeners (mm^2)\n",
- "t=2 #thickness (mm)\n",
- "I=2000 #second moment of area (mm^4)\n",
- "w=5\n",
- "#eqn 9.29 tan(a)^4=(1+td/2A_F)/(1+td/2A_S)\n",
- "alpha=math.atan(((1+t*h/2/A_f)/(1+t*l1/A_s))**0.25)\n",
- "\n",
- "#eqn 9.19\n",
- "F_T=w*L/h+w/2/math.tan((alpha))\n",
- "\n",
- "#eqn 9.25 M_max=w*b^2*tan(a)/12/d\n",
- "M_max=w*10**3*l1**2*math.tan(alpha)/12/h\n",
- "print \"maximum value of bending moment = %1.1e N.mm \\n\"%(M_max)\n",
- "\n",
- "#eqn 9.23 P=w*b*tan(a)/d\n",
- "P=w*l1*math.tan(alpha)/h\n",
- "print \"compressive load in stiffener = %1.1f kN \\n\"%(P)\n",
- "\n",
- "#eqn 9.24 le=d/(4-2b/d)^0.5\n",
- "le=h/(4-2*l1/h)**0.5\n",
- "print \"equivalent length of stiffener = %3.1f mm\\n\"%(le)\n",
- "\n",
- "#eqn 8.7 Pcr=pi^2*E*I/le^2\n",
- "P_CR=math.pi**2*E*I/le**2\n",
- "print \"buckling load of a stiffener = %2.1f kN \\n\"%(P_CR) #approx. value in book"
- ],
- "language": "python",
- "metadata": {},
- "outputs": [
- {
- "output_type": "stream",
- "stream": "stdout",
- "text": [
- "maximum value of bending moment = 8.6e+04 N.mm \n",
- "\n",
- "compressive load in stiffener = 3.4 kN \n",
- "\n",
- "equivalent length of stiffener = 253.0 mm\n",
- "\n",
- "buckling load of a stiffener = 21589.8 kN \n",
- "\n"
- ]
- }
- ],
- "prompt_number": 13
- },
- {
- "cell_type": "code",
- "collapsed": false,
- "input": [],
- "language": "python",
- "metadata": {},
- "outputs": []
- }
- ],
- "metadata": {}
- }
- ]
-}
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