blob: 09d5175d727cf08576b066b24b8da36bad5da867 (
plain)
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
|
// Problem no 9.10,Page no.240
clc;clear;
close;
L=3 //m //Length of strut
b=0.04 //m //Width of rectangle
d=0.10 //m //Depth if rectangle
P=100*10**3 //N //Axial thrust
w=10*10**3 //N //Uniformly Distributed Load
E=210*10**9 //Pa
//Calculations
A=b*d //m**2 //Area of strut
I=b*d**3*12**-1 //m**4 //M.I
m=(P*(E*I)**-1)**0.5
//Let X=secmL*2**-1
X=(1*(cos(m*L*2**-1))**-1)
M=w*E*I*P**-1*(X-1)*3**-1 //N*m //Max Bending Moment
sigma_1=P*A**-1 //Pa //Direct stress
sigma_2=M*0.05*I**-1 //Pa //Bending stress
sigma_c_max=sigma_1+sigma_2 //Max compressive stress
//If the Eccentricity of thrust is neglected
M_2=w*L**2*(3*8)**-1 //Max Bending moment
sigma_2_2=M_2*0.05*I**-1 //Pa //Bending stress
sigma_c_max_2=(sigma_1+sigma_2_2)*10**-6 //Pa
//Let Y=Percentage error
Y=((sigma_c_max-sigma_c_max_2*10**6)*sigma_c_max**-1)*100
//Result
printf("Max stress induced is %.2f",sigma_c_max_2);printf(" MPa")
printf("\n The Percentage Error is %.3f %%",Y)
|