Challenge

Section Modulus calculation and optimization

SECTION MODULUS OF THE HOOD

Objective: To find the section modulus of the hood and optimisation to improve the overall section modulus.

Section Modulus: The section modulus (S) is geometric property of the cross section used for designing beams and flexural members. It does not represent anything physically.

Formula of Section Modulus: It may be defined as the ration of total moment resisted by the section to the stress in the extreme fibre which is equal to yield stress.

        There fore

          S = I/Y, Where

S = Section modulus (mm^3)

I = Moment of Inertia of the section about the bending axis. (mm^4)

Y = Distance between the neutral axis and extreme end of the object (mm)

Area moment of Inertia:

The area moment of inertia of a beams cross sectional area measures the beam ability to resist bending.  The larger the moment of inertia less will be the bend.

Where,

M = Bending moment

I = Area moment of Inertia

E = Youngs modulus

R = Radius of gyration

Neutral axis: When beam is subjected to pure bending the top most fibres of the beam are subjected to maximum compression, while the bottom most fibres of the beams are subjected to maximum tension.

Calculation:

Frontal crash:

Itration-1:

Itration-2:

Front crash 2mm offset:

Side crash:

Itration-1

Itration-2

side crash 2mm offset:

Section view:

Observation:

SECTION MODULUS DATA FRONT CRASH ORIGINAL FRONT CRASH 2MM SIDE CRASH ORIGINAL SIDE CRASH 2MM
Imin(in meters) 2.186*10^6 2.619*10^6 6.599*10^7 8.216*10^7
Imax(in meters) 7.63*10^8 8.92*10^8 1.295*10^8 1.529*10^8
I min(in mm) 2186000 2619000 659900 821600
I max(in mm) 763000000 892000000 129500000 152900000
Total distance(in mm) 875.176 874.615 484.373 484.152
Y=Total dis/2 (in mm) 437.588 437.307 242.186 242.076
S min= I min/y(in mm) 4.995.566 5.988.927 2.724.765 3.393.975
S max= I max/y (in mm) 1.743.649.277 2.039.756 47.527.034 631.619.821
S avg=(Smin+Smax)/2(in mm) 874.322.421.5 4.014.341.5 25.125.899.5  317.506.898

sample calculation:

Itration-1

Frontal crash original:

Imin(in meter)=2.186*10^6 m

Imax(in meter)=7.63*10^8m

Imin (in mm)= 2186000 mm

Imax (in mm)= 763000000 mm

Total distance = 875.176mm

Y=total distance/2 =437.588 mm

S=I/Y

Smin=Imin/y

Smax=Imax/Y

Smin = 2186000/437.588 = 4.995.566 mm

Smax = 763000000/437.588 = 1.743.649.277 mm

S avg =(Smin + Smax)/2

         =(4.995.566+1.743.649.277)/2

         =874.322.421.5 mm

Itration-2

Frontal crash 2 mm offset:

Imin(in meter)=2.619*10^6

Imax(in meter)=8.92*10^8

Imin (in mm)= 2619000 

Imax (in mm)= 892000000

Total distance =874.615

Y=total distance/2 =437.307

S=I/Y

Smin=Imin/y

Smax=Imax/Y

Smin = 2619000/437.307 

         =5.988.927

Smax = 892000000/437.307

          =2.039.756

S avg =(Smin + Smax)/2

         =(5.988.927+2.039.756)/2

         =4.014.341.5

By comparing the both the cases

 874.322.421.5< 4.014.341.5

Conclusion:

The section modulus value for the offset range  of 2 mm of the inner panel of the hood has the maximum value when compared to the original dimension. I conclude that the section modulus increases the stress will be decreased. If we design in this method we can achieve the structure.

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