Establishing Neutral Axis & Second Moment on a T bar beam

In summary, the conversation discusses a difficulty in finding the second moment of area and neutral axis of a beam. Different formulas are suggested and calculations are shown, leading to a final calculation for the second moment of area of 1827mm. The conversation also touches on the topic of stress and strain at the neutral axis. Book recommendations are given for further understanding.
  • #1
amjid1709
22
0

Homework Statement



I'm having difficluty in finding the second moment of area and neutral axis of this beam can anyone help

Homework Equations





The Attempt at a Solution



I know that you have to divide the beam into two rectangles, I have used the formula bd3/12 and Izz, i did Izz = (1/12)6.4(38.1)^3 and the answer came to 29496.72

surely this can't be right I am going wrong somewhere, can anyone help, it hasnt got to be in for a few weeks but I want to do this now.

Can anyone help, I have attached the dimensions of the beam
 

Attachments

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  • #2
I have seen the question similar to mine by struggling but that does not explain it.

Can anyone please help?
 
  • #3
You may want to describe the section of the beam, or post it on a photo album site, because the document appears to be waiting for approval.
 
  • #6
I understand all of that but what figure is d0 it says it is the distance of the central axis but if i multiply a larger number comes up.
 
  • #7
It would be much easier if you could post what you have attempted to do, so I can see how you arrived at your answer, or the problem of the 'large number'.
 
  • #8
Thanks for getting back to me,

The figures I'm getting are 38.1 X 6.4 (243.84) + 31.7*6.4 (202.88)which is 446.72 this is fine as it is adding the two rectangles up however if I multiply like what Kazza said by 15.1 it gives me 6745.472, I am no where near the figure of 11.85 he got.

The other formula I have is

A X d + A2 X d2 divide by Area 1 + Area 2

dont know which one I should use but I'm not getting 11.85 which seems to be the correct answer as it seems logical it may be right but I don't feel comfortable in just copying what his wrote because I don't know where he has got the figures from.

Thanks
 
  • #9
The 11.85 he got was measured from the bottom edge of the flange (horizontal rectangle).

All you need to do is to split the shape into two rectangles, namely the flange of 6.4*38.1 and the web of 6.4*31.7, as you mentioned. The 446.72 you obtained is perfect for the total area.

Now you need to take moments of each area about the reference line, i.e. bottom edge of the flange, i.e. calculate [tex]\Sigma[/tex]AiDi.
You have already calculated Ai of the individual rectangles.
Now you need the distance of the centroid of each rectangle from the reference line.

Divide this sum by 446.72 (sum of areas) should give you 11.85 as you expected.
 
  • #10
Sorry but I still can't do it, what do you eactly mean by moments of the refrence line,

is it 243.84 * 3.2 + (202.88 * 15.85) + 6.4 = 4002.336

if I divide that by 446.72 it gives 8.95 still not close enough what am I doing wrong.
 
  • #11
By the way the 15.85 is my refrence line which is the centroid
 
  • #12
any body?
 
  • #13
Thanks mathmate, your guidance has enabled me to crack the question I now have the answer to 11.85 and do undersatnd it now.

Just another question how do you calculate the strain at the neutral axis, do i need to use another formula for this?
 
  • #14
Yes, you'd need another formula to calculate the stress, [tex]\sigma[/tex], at different places in the section.
Stress is defined as force divided by the area, and strain,[tex]\epsilon[/tex], is the unit deformation, i.e. deformation divided by the length.
In the absence of axial forces, the stress at the neutral axis is zero, therefore the strain also.
The stress,[tex]\sigma[/tex], is given by the formula:
[tex]\sigma[/tex]=Mc/I, where
M=bending moment,
I=moment of inertia of cross section, and
c=distance from neutral axis.

This means that the further away from the neutral axis, the greater is the stress. This formula assumes plane stress, meaning that the deformations across the section remain in a plane.

The strain at different points is simply
[tex]\epsilon[/tex] = [tex]\sigma[/tex]/E, where E is the modulus of elasticity.

You said you have obtained the neutral axis. Did you calculate the moment of inertia of the section? What did you get?

Just a side question: do you have any textbooks on Strength of Materials? If not, I can recommend a few that you can certainly get from the library:

Strength of Materials, by Stephen Timoshenko (the classic, but rather expensive)
https://www.amazon.com/dp/0898746213/?tag=pfamazon01-20

Strength of Materials, by J. P. Den Hartog, an excellent work, available in Dover edition
https://www.amazon.com/dp/0486607550/?tag=pfamazon01-20

Strength of Materials, By Pytel and Singer, a standard textbook, very affordable.
https://www.amazon.com/dp/0060453133/?tag=pfamazon01-20
 
  • #15
Thanks for the info about the books I have checked the uni library website and they are available to borrow so will do that monday.

Did you mean second moment of area?
 
  • #16
You're right, it's second moment of area that I meant.

Many engineers refer to the second moment of area as the moment of inertia and use the same symbol I for both, which may be confusing.

Sorry I fell into that bad habit, as quoted in Wiki
http://en.wikipedia.org/wiki/Second_moment_of_area
It continued to say:
Which inertia is meant (accelerational or bending) is usually clear from the context and obvious from the units: second moment of area has units of length to the fourth power whereas moment of inertia has units of mass times area.
which made me feel better!
 
  • #17
Second Moment of Area using parallel axis theorem

I = Bd3
12

Rectangle A

Y = 6.4 + 38.1 -11.85
2
Y= 13.6

Bd3 + (13.6)2
12

= 1017.2mm4

Rectangle B

Y = 6.4 + 31.7 -11.85
2
Y= 10.85

Bd3 + (10.85)2
12

= 810.2mm4

Total Second moment of area = 1827mm

is this correct?
 
  • #18
The second moment of area of a rectangle is
I=bd3/12
where b is the dimension parallel to the axis passing through the centroid, and
d is the dimension perpendicular to the centroid.
In the example given, rectangle A has a dimension of 38.1 and height of 6.4. The axis is horizontal passing through the centre of the rectangle at 3.2 from the bottom edge.
So
b=38.1 (parallel to horizontal axis)
d=6.4 (perpendicular to axis)
and
Ia=38.1*6.43/12=832.3072
Ib=second moment of inertia of rectangle (31.7*6.4) B
Let
Aa=area of rectangle A = 38.1*6.4=243.84
Ya=distance of centroid of rectangle A from bottom flange= (6.4/2)=3.2
Ab=area of rectangle B
Yb=distance of centroid of rectangle B from bottom flange
The distance of centroidal axis from the bottom flange (bottom of rectangle A)
y=(Aa*Ya+Ab*Yb)/(Aa+Ab)=11.85 (as calculated before)

The parallel axis theorem states that the second moment of area about an axis
parallel and at a distance d from the centroidal axis is
I'=Ic+A*d2
Ic=second moment of inertia about its centroidal axis
I'=second moment of inertia about the new axis.

So the Total second moment of area is
I=Ia+Aa*(Ya-y)2+Ib+Ab*(Yb-y)2
=5#00#.865

# represents a missing digit.

There should be enough information for you to proceed with your calculations. In addition, here is a link that shows you how to tabulate your calculations, and hence minimizing errors.
http://www.cen.bris.ac.uk/personal/cenaa/Nick's Web site/notes/Mechanics I/tutorial.pdf
 
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  • #19
Thank you very much for that, I'm starting to learn it now may be you should consider being a lecturer, you have done more explaining than my own lecturers.

I will have a go at that tonight, by the way the link you pasted does not work it says its a unkown file.

Would it be possible to repaste it, thanks once again, you have been very kind.
 
  • #20
Thank you for the appreciation. It's a pleasure to know that my help is of some use.

Perhaps the site was down at the moment you tried it. I tried it a moment ago and it worked.
Also, if you copy and paste, it may not work, because it will be missing a few details. You just have to double click on the link. If you are worried about double-clicks, you can hover over the link, and copy by hand on the bottom left, of the window, which gives you the complete address without double-clicking. (that works for firefox, probably IE as well).

Here it is again, just in case.
http://www.cen.bris.ac.uk/personal/cenaa/Nick's Web site/notes/Mechanics I/tutorial.pdf
 
Last edited by a moderator:
  • #21
Am I correct in saying Yb is the distance of centroid of rectangle B from bottom flange which I have calculated it to be 15.85?

and also which you stated Ib=second moment of inertia of rectangle (31.7*6.4) B

is this 31.7 *6.4 Xy3 /12

which equals to 692.497
 
  • #22
In my calculations, all distances are measured from the bottom of the bottom flange, which makes the centroid of rectangle A 6.4/2=+3.2, and
Yb=31.7/2+6.4=22.25

Ib=second moment of inertia of rectangle (31.7*6.4) B
Sorry about the above line, it should read:

Ib=second moment of inertia of rectangle about its centroid.

because I wanted you to calculated it.
It should be the width multiplied by the cube of the depth, and divided by 12.
 
  • #23
This is what I'm getting over and over again.

(832.3072 + 243.84) * (3.2 -11.85)2 + (692.49 +202.88) * 108.16

1076.1472 * 74.8225 + 895.37 *108.16

= 8805887.38

this isn't right and I have not got a clue where I'm going wrong.
 
  • #24
(832.3072 + 243.84) * (3.2 -11.85)2 + (692.49 +202.88) * 108.16
The parallel axis theorem (I'=Ic+A*d2) applies to the individual rectangles. You seem to be adding up the second moment of area (832.3072) to the area (243.84) which does not have the same unit. You may want to do

I=832.3072 + 243.84*(3.2 -11.85)2 + I2 +202.88*(Yb-11.85)2

You have to recalculate I2 using the formula I2=bh3/12, where b=6.4 & h=31.7
As discussed before, Yb=31.7/2+6.4, being the distance of the centroid of rectangle B from the bottom of the flange.

You're almost there.
 
  • #25
Thanks for that Mathmate, I will try and do it today a family emergency has risen and I will try and do it tonight.

Please keep in contact once I have done it I will get back to you.

Many thanks, could'nt have done it without your assistance.
 
  • #26
If you have time, a revision on the subject after getting books from the library will do you good for the exams. What we have gone through is one problem. To be able to solve other problems, you need to do more reading, more understanding, and more exercises.
 

What is a T bar beam?

A T bar beam is a type of structural beam that is shaped like the letter "T". It is commonly used in construction and engineering projects to support heavy loads.

What is the neutral axis of a T bar beam?

The neutral axis of a T bar beam is an imaginary line that divides the beam into two equal parts, with one part being in tension and the other in compression. It is the point where the internal stresses of the beam are neutralized.

How is the neutral axis of a T bar beam determined?

The neutral axis of a T bar beam can be determined by analyzing the cross-sectional properties of the beam, such as its moment of inertia and cross-sectional area. It can also be determined experimentally by applying a load to the beam and observing the deflection.

What is the second moment of a T bar beam?

The second moment, also known as the moment of inertia, is a measure of the beam's resistance to bending. It is a crucial parameter in determining the strength and stiffness of the beam.

How is the second moment of a T bar beam calculated?

The second moment of a T bar beam can be calculated using mathematical equations that take into account the cross-sectional properties of the beam, such as its width and height. It can also be calculated experimentally by measuring the deflection of the beam under a known load.

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