Stress analysis -- derive equations: bending & yielding

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Discussion Overview

The discussion revolves around deriving equations related to stress analysis, specifically focusing on bending and yielding in materials. The context includes mechanical behavior of materials and design optimization, with an emphasis on stiffness and strength in the evaluation of different materials.

Discussion Character

  • Exploratory, Technical explanation, Homework-related

Main Points Raised

  • One participant, an alloy chemist, expresses difficulty in deriving equations for a problem related to plane stress and stiffness, indicating a background in materials engineering.
  • Another participant suggests that the problem involves a simple beam in bending but requests more information to clarify the questions posed.
  • A third participant notes that the panel in question may be stiffer than a typical beam due to its inability to contract laterally, and discusses the potential goal of optimizing mass while maintaining stiffness and strength.
  • This participant also mentions the importance of starting with a free body diagram and suggests drawing shear and moment diagrams to analyze the stress at the bottom of the panel.
  • The original poster indicates that the example will be used to compare materials, factoring in cost and production processes, and expresses a desire to understand the variables involved in deriving the necessary equations.

Areas of Agreement / Disagreement

Participants have not reached a consensus on the specifics of the problem or the equations needed. Multiple viewpoints on the nature of the problem and the approach to solving it remain present.

Contextual Notes

There are limitations in the information provided, including a lack of detailed problem statements and definitions of terms like "bending momentum." The discussion also reflects varying levels of familiarity with the concepts involved.

Who May Find This Useful

This discussion may be useful for students and professionals in materials engineering, mechanical engineering, and related fields who are interested in stress analysis and material properties.

Strife_Cloud
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Problem attached.

I would appreciate anyone's help. I am an alloy chemist working on an MS degree in materials engineering and have come to the mechanical engineering part of the program and am feeling a bit behind. Deriving an equation for this case is proving to be difficult for me although I believe we are still at the elementary mechanical review period.

The basic situation is that of plane stress with an "important focus" on stiffness. The class is following the mechanical behavior of materials book by Dieter. I have a lot of time putting the pieces together but an now a bit stumped.
 

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All you appear to have in this problem is a simple beam in bending but I can't make much sense of the actual questions at all .

Have you any more information ?
 
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Nidum said:
All you appear to have in this problem is a simple beam in bending

With the subtlety that this panel will be stiffer than a beam because it cannot contract laterally (because of its large width). I wrote a summary of generalized[/PLAIN] Hooke's Law for solving problems like this. It looks like the questions are essentially aiming at a design optimization problem in which the mass of the panel might be minimized while maintaining a given stiffness (in (b)) and strength (in (c))? But "bending momentum" is not a term I'm familiar with; I suppose it's meant to mean the bending moment.

Strife_Cloud, I'd start with a free body diagram of the panel. Have you covered shear and moment diagrams? If so, draw these too. Then find the stress at the bottom of the panel at the middle.
 
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Yes, we are going to be using this example to compare different materials and focus on what material we should consider. Then factoring in cost of materials and what processes are involved in production and how that leads to the properties of the final product.

The image is what he posted online to be completed before class. Adding that, we would use the equations we derive evaluating materials for the depicted stress state.

Unfortunately, that is all the information given on the sheet so I have been attempting to go through all of the variables we have been given hoping the combination leading to the equation will click but, it hasn't yet. I look forward to reading the information on the link provided and I will let you know how it helps! Thank you both for responding and for your help!
 

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