Calculating the bending stress of a simply supported beam

In summary, In FEA, we use the maximum bending moment at all points along the beam to calculate the bending stress.
  • #1
tomtomtom1
160
8
TL;DR Summary
Calculating Bending Stress Of A Member
Hello all

I am trying to calculate the bending stress of a simply supported beam with a load of 12kn at the middle of a 6m span, member depth of 0.016m

I have drawn both the bending moment and shear force diagram.

I want to know the following:-

1) When calculating the bending stress would you always use the Max bending moment Or would you use the bending moment at a particular point along the member? below is a sketch:-

m1.JPG


As you can see i have calculated the bending stress at 1m along the beam - is it convention to always use the max bending moment at all points along the beam or the actual bending moment at the point along the beam to which your calculating the bending stress for?

As you can see i have 2 answers and i am not sure which is correct?

2) How would you know that the value i get for bending stress is compressive or tensile, i think that i get a positive value which is compressive because i went 0.008m UP my neutral axis which is in compression - would this be correct?

Thank you.
 
Engineering news on Phys.org
  • #2
We pretty much always calculate bending stress at a point along the beam where bending moment (and thus also stress) is highest. So in the case of simply supported beam with force in the middle this point will be in the middle of the beam. The formula for bending stress includes vertical distance from neutral axis. Bending stress is maximum in extreme (outer) fibers so we take the distance from neutral axis to points of the cross section farthest away from this axis.
Now when it comes to the sign, in this case stresses above neutral axis will be compressive while those below the neutral axis will be tensile.
 
  • Like
Likes tomtomtom1 and berkeman
  • #3
FEAnalyst said:
We pretty much always calculate bending stress at a point along the beam where bending moment (and thus also stress) is highest. So in the case of simply supported beam with force in the middle this point will be in the middle of the beam. The formula for bending stress includes vertical distance from neutral axis. Bending stress is maximum in extreme (outer) fibers so we take the distance from neutral axis to points of the cross section farthest away from this axis.
Now when it comes to the sign, in this case stresses above neutral axis will be compressive while those below the neutral axis will be tensile.

FEAAnalyst.

Thanks

Just out of interest what FEA software do you use?

I wanted to start using one but wasnt sure which one would be the easiest to learn just as a starter.

A few people are using Solidworks.

Thoughts?

Thanks
 
  • #4
I use several FEA programs but mainly Abaqus (on a daily basis). It's not as intuitive for beginners as other software but has really huge capabilities. In my opinion Abaqus is the best choice for structural mechanics. I work in SolidWorks Simulation too. This one is good for people starting their adventure with FEA. It has some significant limitations but is really powerful for a CAD-embedded FEA module.
 
  • Like
  • Informative
Likes tomtomtom1, jrmichler and berkeman
  • #5
I have also used both Abaqus and SolidWorks Simulation. SolidWorks is all that I ever needed for machine design linear static analyses. After, that is, I identified the limitations and developed work arounds. SolidWorks is particularly weak on problems with contact, but almost all machine design and structural problems can be solved without using contact.

A problem like the Howe truss in this thread would be trivial in SolidWorks: https://www.physicsforums.com/threa...s-2d-pinned-at-both-ends.981939/#post-6278877.

In order to use FEA effectively, it is absolutely necessary to have a solid understanding of basic stress, strain, FBD, moment, shear, etc concepts.
 
  • Like
Likes tomtomtom1
  • #6
Thank you all.

I think i am going to start with solid works to being with and at the same time continue to learn the basics.

I have now started by adventure into the FEA :)

Thank you.
 
  • Like
Likes jrmichler

What is the formula for calculating bending stress of a simply supported beam?

The formula for calculating bending stress of a simply supported beam is σ = (M * c) / I, where σ is the bending stress, M is the bending moment, c is the distance from the neutral axis to the outermost fiber, and I is the moment of inertia of the beam's cross-sectional area.

What are the units of measurement for bending stress?

Bending stress is typically measured in units of force per unit area, such as pounds per square inch (psi) or newtons per square meter (Pa).

How does the length of a beam affect bending stress?

The longer the beam, the greater the bending stress will be. This is because longer beams have a larger moment of inertia, which means they are less resistant to bending forces.

What is the maximum allowable bending stress for a simply supported beam?

The maximum allowable bending stress for a simply supported beam depends on the material the beam is made of. It is typically determined by the yield strength of the material, which is the maximum stress the material can withstand before permanent deformation occurs.

How can I reduce bending stress in a simply supported beam?

There are several ways to reduce bending stress in a simply supported beam, including using a stronger material, increasing the beam's cross-sectional area, or decreasing the length of the beam. Additionally, adding support or reinforcement to the beam can also help reduce bending stress.

Similar threads

  • Mechanical Engineering
Replies
30
Views
4K
  • Mechanical Engineering
2
Replies
36
Views
3K
  • Mechanical Engineering
Replies
3
Views
1K
  • Mechanical Engineering
Replies
1
Views
2K
  • Mechanical Engineering
Replies
1
Views
2K
  • Mechanical Engineering
Replies
1
Views
907
Replies
2
Views
1K
  • Mechanical Engineering
Replies
9
Views
1K
  • Mechanical Engineering
Replies
3
Views
2K
  • Mechanical Engineering
Replies
1
Views
3K
Back
Top