diff options
Diffstat (limited to '3772/CH9/EX9.10')
-rw-r--r-- | 3772/CH9/EX9.10/Ex9_10.sce | 39 |
1 files changed, 39 insertions, 0 deletions
diff --git a/3772/CH9/EX9.10/Ex9_10.sce b/3772/CH9/EX9.10/Ex9_10.sce new file mode 100644 index 000000000..09d5175d7 --- /dev/null +++ b/3772/CH9/EX9.10/Ex9_10.sce @@ -0,0 +1,39 @@ +// 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) |