Axial loading of a composite beam

In summary, the conversation is about a problem involving axial loads on a bar made of brass and steel. The first part of the solution is confirmed to be correct, but there is confusion in the second part regarding the inclusion of a compressive force. The conversation also discusses the effects of the yield stress of brass on the solution. The final solution involves calculating the compressive forces on both the brass and steel rods, and determining the stresses on each material.
  • #1
ski0331
10
0

Homework Statement


PAokWiX

PAokWiX.jpg

Homework Equations


In my attempt at a solution

The Attempt at a Solution


eCRKbcI
eCRKbcI.jpg
 

Attachments

  • PAokWiX.jpg
    PAokWiX.jpg
    36.6 KB · Views: 1,763
  • eCRKbcI.jpg
    eCRKbcI.jpg
    44.7 KB · Views: 982
Physics news on Phys.org
  • #2
Basically I'm asking if I did this correctly and have the correct answer and if I don't, what I did wrong and where I went wrong in my thinking.
 
  • #3
I confirm the result in the first part, but I don't follow what you did in the 2nd part. It seems to me for the 2nd part, all you need to do is add a compressive force to the entire rod that compresses it 13.04 mm: $$\frac{FL_1}{A_1E_1}+\frac{FL_2}{A_2E_2}=-0.01304$$
 
  • #4
Where did you get the 13.04 mm? And I thought I did add them together f=-ax and f2=-ax+4000N
 
  • #5
ski0331 said:
Where did you get the 13.04 mm? And I thought I did add them together f=-ax and f2=-ax+4000N
I'm just doing it as 2 superimposed problems. In the first part, you showed that the growth of the bar would be 14.04 mm if the bar were totally unconstrained. Since the original gap was 1 mm, that would mean that you would have to compress the bar 13.04 mm to get it to fit into the available space.

Assuming purely elastic behavior, this gives a compressive stress of 106 MPa in the Brass and a compressive stress of 131 MPa in the steel. But the yield stress of the Brass is only 78 MPa. How do you think that would affect the answer?
 
Last edited:
  • #6
Chestermiller said:
I'm just doing it as 2 superimposed problems. In the first part, you showed that the growth of the bar would be 14.04 mm if the bar were totally unconstrained. Since the original gap was 1 mm, that would mean that you would have to compress the bar 13.04 mm to get it to fit into the available space.

Assuming purely elastic behavior, this gives a compressive stress of 106 MPa in the Brass and a compressive stress of 131 MPa in the steel. But the yield stress of the Brass is only 78 MPa. How do you think that would affect the answer?
I'm not sure. would it? I've struggled with this subject (axial loads). But a guess would be that it would bend the brass?
 
  • #7
ski0331 said:
I'm not sure. would it? I've struggled with this subject (axial loads). But a guess would be that it would bend the brass?
When you complete the solution of the purely elastic problem and have confirmed my answer, we can talk about what to do because the compressive yield stress of the brass is reached.

Your solution for the elastic problem is incorrect because you included the 4000 with the steel rather than with the brass.
 
  • #8
Chestermiller said:
When you complete the solution of the purely elastic problem and have confirmed my answer, we can talk about what to do because the compressive yield stress of the brass is reached.

Your solution for the elastic problem is incorrect because you included the 4000 with the steel rather than with the brass.
ahhh ok I see where I did that! That makes sense, but I make my first cut to determine what Ax is for my free body diagram before the 4Kn. Like I said axial loads have been giving me fits to solve.
 
  • #9
ski0331 said:
ahhh ok I see where I did that! That makes sense, but I make my first cut to determine what Ax is for my free body diagram before the 4Kn. Like I said axial loads have been giving me fits to solve.
OK. Let's see what you get now. It seemed to me you were doing pretty well up to this point.
 
  • #10
Chestermiller said:
OK. Let's see what you get now. It seemed to me you were doing pretty well up to this point.
7E12OPt.png
 

Attachments

  • 7E12OPt.png
    7E12OPt.png
    5.9 KB · Views: 815
  • #11
ski0331 said:
No. You need to be careful with your arithmetic: $$-\frac{(A_x+4000)(10)}{(101\times 10^9)(100\times 10^{-6})}-\frac{(A_x)(10)}{(200\times 10^9)(50\times 10^{-6})}+0.018=0.001$$ where ##A_x## is a positive compressive force. What do you get for ##A_x##? What do you get for F from my equation in post #3?
 
  • #12
Chestermiller said:
No. You need to be careful with your arithmetic: $$-\frac{(A_x+4000)(10)}{(101\times 10^9)(100\times 10^{-6})}-\frac{(A_x)(10)}{(200\times 10^9)(50\times 10^{-6})}+0.018=0.001$$ where ##A_x## is a positive compressive force. What do you get for ##A_x##? What do you get for F from my equation in post #3?
A(x) I got is equal to 6552.24, F=-6552.44
 
  • #13
ski0331 said:
A(x) I got is equal to 6552.24, F=-6552.44
I confirm. I treated F as tension and got a negative number, while you treated it as compression and got a positive number. So this is the compressive force on the steel rod, and the compressive force on the brass rod is 6552+4000=10552 N. What do these solutions to the elastic problem (neglecting the yield stress) give you for the stresses in the brass and the steel?
 
  • #14
Chestermiller said:
I confirm. I treated F as tension and got a negative number, while you treated it as compression and got a positive number. So this is the compressive force on the steel rod, and the compressive force on the brass rod is 6552+4000=10552 N. What do these solutions to the elastic problem (neglecting the yield stress) give you for the stresses in the brass and the steel?
uvwIKkq.png
 

Attachments

  • uvwIKkq.png
    uvwIKkq.png
    8.5 KB · Views: 881
  • #16
  • #17
ski0331 said:
ok you lost me on this chart. why are there 4p? 2 ax?
The forces on the left are the reaction forces from the constraint. The 2 P forces on the right are the applied forces. The Ax on the right is the compressive force applied on the brass section by the steel section.

You are aware that tension and compression are bi-directional, arising from the application of the Cauchy stress relationship to determine the forces acting on a surface? You remember from freshman physics the tension in a rope pointing to the right (for the force the material on the right applies to the material on the left), and to the left (for the force the material on the left applies to the material on the right), correct?
 
  • #18
Chestermiller said:
The forces on the left are the reaction forces from the constraint. The 2 P forces on the right are the applied forces. The Ax on the right is the compressive force applied on the brass section by the steel section.

You are aware that tension and compression are bi-directional, arising from the application of the Cauchy stress relationship to determine the forces acting on a surface? You remember from freshman physics the tension in a rope pointing to the right (for the force the material on the right applies to the material on the left), and to the left (for the force the material on the left applies to the material on the right), correct?
yes but Ax is the reaction forces of the wall. In my FBD Ax pushes back on 2p and the Normal force.
 
  • #19
ski0331 said:
yes but Ax is the reaction forces of the wall. In my FBD Ax pushes back on 2p and the Normal force.
Taking each section as a free body, the forces on the two ends of each section must be equal in magnitude and opposite in direction. Otherwise, the sections could not each be in force equilibrium.
 
  • #20
An overall force balance on the composite beam tells you that the reaction force on the left boundary has to be ##A_x+2P##.
 

1. What is axial loading of a composite beam?

Axial loading is a type of force applied to a composite beam that runs along its length, causing it to deform or bend. This can be either a compressive force, pushing the beam together, or a tensile force, pulling the beam apart.

2. How does axial loading affect the strength of a composite beam?

Axial loading can significantly impact the strength of a composite beam. When the beam is under compressive loading, it may buckle or fail due to buckling. Tensile loading can cause the beam to elongate and ultimately fail due to tensile stress.

3. What factors influence the response of a composite beam to axial loading?

Several factors can affect how a composite beam responds to axial loading, including the material properties of the beam, the cross-sectional shape and size, the type of loading (compressive or tensile), and the boundary conditions.

4. How is the maximum axial load a composite beam can withstand determined?

The maximum axial load a composite beam can withstand is determined through various analytical and experimental methods. These include calculating the buckling load using equations, performing physical tests on the beam, and using computer simulations to model the behavior of the beam under different loading conditions.

5. How can the strength of a composite beam be improved to resist axial loading?

To improve the strength of a composite beam against axial loading, various design techniques can be used. These include increasing the cross-sectional area of the beam, using materials with higher strength and stiffness, and incorporating reinforcement elements such as braces or trusses.

Similar threads

  • Engineering and Comp Sci Homework Help
Replies
4
Views
2K
  • Engineering and Comp Sci Homework Help
Replies
2
Views
661
  • Engineering and Comp Sci Homework Help
Replies
3
Views
354
  • Engineering and Comp Sci Homework Help
Replies
1
Views
1K
  • Engineering and Comp Sci Homework Help
Replies
3
Views
587
  • Engineering and Comp Sci Homework Help
Replies
8
Views
2K
  • Engineering and Comp Sci Homework Help
Replies
5
Views
1K
  • Engineering and Comp Sci Homework Help
Replies
4
Views
82
  • Engineering and Comp Sci Homework Help
Replies
4
Views
824
  • Engineering and Comp Sci Homework Help
Replies
3
Views
1K
Back
Top