Chapter 22: Fuselages

Example 22.1 Pg.No.598

In [9]:
from __future__ import division
import math
#B1=t_D*b/6(2+sigma_2/sigma_1)
Mx=200*10**6                     # (N*mm)
y=[381,352,269.5,145.8,0,-145.8,-269.5,-352,-381,-352,-269.5,-145.8,0,145.8,269.5,352]
sigma_2=sigma_16=352
sigma_1=381
A=100
B1=A+0.8*149.6/6*(2+sigma_2/sigma_1)*2
Ixx=2.52*10**8
def sigma_z(y):
    return Mx/Ixx*y
print "Stringer/Boom \t y(mm) \t \tsigma_z(N/mm^2)"
for i in range (0,16):
    print "%2.0f \t\t %3.1f\t\t\t%3.1f "%(i+1,y[i],sigma_z(y[i]))
Stringer/Boom 	 y(mm) 	 	sigma_z(N/mm^2)
 1 		 381.0			302.4 
 2 		 352.0			279.4 
 3 		 269.5			213.9 
 4 		 145.8			115.7 
 5 		 0.0			0.0 
 6 		 -145.8			-115.7 
 7 		 -269.5			-213.9 
 8 		 -352.0			-279.4 
 9 		 -381.0			-302.4 
10 		 -352.0			-279.4 
11 		 -269.5			-213.9 
12 		 -145.8			-115.7 
13 		 0.0			0.0 
14 		 145.8			115.7 
15 		 269.5			213.9 
16 		 352.0			279.4 
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