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) 1.772*10^6 2.172*10^6 1.044*10^6 1.252*10^6
Imax(in meters) 6.501*10^8 7.74*10^8 1.454*10^8 1.682*10^8
I min(in mm) 1772000 2172000 1044000 1252000
I max(in mm) 650100000 774000000 145400000 168200000
Total distance(in mm) 878.998 878.646 485.15 484.927
Y=Total dis/2 (in mm) 439.499 439.323 242.575 242.4635
S min= I min/y(in mm) 4031.86355 5522.17897 4303.82356 5163.66381
S max= I max/y (in mm) 1479184.25 1761801.68 599402.247 693712.662
S avg=(Smin+Smax)/2(in mm) 741608.055 883661.93 301853.036 349438.163

sample calculation:

Itration-1

Frontal crash original:

Imin(in meter)=1.772*10^6 m

Imax(in meter)=6.501*10^8m

Imin (in mm)= 1772000 mm

Imax (in mm)= 650100000 mm

Total distance = 878.998mm

Y=total distance/2 =439.499 mm

S=I/Y

Smin=Imin/y

Smax=Imax/Y

Smin = 1772000/439.499 =4031.86355 mm

Smax = 650100000/439.499 = 1479184.25 mm

S avg =(Smin + Smax)/2

=(4031.86355+1479184.25)/2

=741608.055 mm

Itration-2

Frontal crash 2 mm offset:

Imin(in meter)=2.172*10^6

Imax(in meter)=7.74*10^8

Imin (in mm)= 2172000

Imax (in mm)= 774000000

Total distance =878.646

Y=total distance/2 =439.323

S=I/Y

Smin=Imin/y

Smax=Imax/Y

Smin = 2172000/439.323

Smax = 774000000/439.323

S avg =(Smin + Smax)/2

=(5522.17897+1761801.68)/2

=883661.93

By comparing the both the cases

741608.055 < 883661.93

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 section modulus increases the stress will be decreased. If we design in this method we can achieve the structure.

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