How to calculate if a part will fail at a specific spot

  • Thread starter Thread starter ENGBIO
  • Start date Start date
  • Tags Tags
    Specific
AI Thread Summary
To determine if a part will fail at specific spots, especially when angled, one cannot solely rely on traditional shear and bending diagrams due to the presence of stress concentrations. Finite Element Analysis (FEA) is essential for accurately calculating von Mises stress at critical locations, which must then be compared to the material's yield stress to assess potential failure. Hand calculations can provide overall stress levels for inclined or horizontal beams, but they are inadequate for sharp corners where stress concentrations occur. Additional details about the structure, including size, material, and external forces, are necessary for a comprehensive analysis. Accurate predictions of stress states in complex geometries require high-quality mesh in FEA.
ENGBIO
Messages
19
Reaction score
1
Hey everybody so I am a student and I am learning about failure analysis. So let's say I have a rigid body that is being kept in this position...there is a moment at A generated by a motor to keep the body in this position, working against the weight of the body itself and small wind force. There are bearing reactions at A. I know about making shear and bending diagrams but when it is angled like this how do I calculate if it will fail at these spots?
moment.png
 
Engineering news on Phys.org
Assumption that the part is rigid can't be made in this case when you want to evaluate failure spots. You could solve this as an inclined beam in bending but it won't account for stress concentrations and these will definitely occur in the spots marked with red dots. You would have to perform Finite Element Analysis to calculate von Mises stress at these locations and then compare it with yield stress of the material to find out if failure may occur due to applied load.
 
  • Like
Likes Chestermiller
FEAnalyst said:
Assumption that the part is rigid can't be made in this case when you want to evaluate failure spots. You could solve this as an inclined beam in bending but it won't account for stress concentrations and these will definitely occur in the spots marked with red dots. You would have to perform Finite Element Analysis to calculate von Mises stress at these locations and then compare it with yield stress of the material to find out if failure may occur due to applied load.
I think I understand. So if it was instead in this position would it then be possible to calculate if it would fail at those points and how?

moment2.png
 
The fact that it's at an angle is not a problem. It can be solved as a beam either way. What I meant is that these hand calculations (for both inclined and horizontal beams) can be used to determine overall stress level due to bending in specific cross-section but they can't account for effects occurring around sharp corners. In these locations there are so called stress concetrations (notch effect). Pretty much only FEA with high quality mesh can predict stress state in such cases. I could perform such analysis for you but I need more details about this structure - its size, material, wind force value and so on. And if you have a picture showing how it looks like in real life then it would be very helpful too.
 
  • Like
Likes AeroGeek
How did you find PF?: Via Google search Hi, I have a vessel I 3D printed to investigate single bubble rise. The vessel has a 4 mm gap separated by acrylic panels. This is essentially my viewing chamber where I can record the bubble motion. The vessel is open to atmosphere. The bubble generation mechanism is composed of a syringe pump and glass capillary tube (Internal Diameter of 0.45 mm). I connect a 1/4” air line hose from the syringe to the capillary The bubble is formed at the tip...
Thread 'Physics of Stretch: What pressure does a band apply on a cylinder?'
Scenario 1 (figure 1) A continuous loop of elastic material is stretched around two metal bars. The top bar is attached to a load cell that reads force. The lower bar can be moved downwards to stretch the elastic material. The lower bar is moved downwards until the two bars are 1190mm apart, stretching the elastic material. The bars are 5mm thick, so the total internal loop length is 1200mm (1190mm + 5mm + 5mm). At this level of stretch, the load cell reads 45N tensile force. Key numbers...
I'd like to create a thread with links to 3-D Printer resources, including printers and software package suggestions. My motivations are selfish, as I have a 3-D printed project that I'm working on, and I'd like to buy a simple printer and use low cost software to make the first prototype. There are some previous threads about 3-D printing like this: https://www.physicsforums.com/threads/are-3d-printers-easy-to-use-yet.917489/ but none that address the overall topic (unless I've missed...
Back
Top