Joint Loaded in Tension: Solving for Component CSA | Step-by-Step Guide

  • Thread starter Thread starter elephunk
  • Start date Start date
  • Tags Tags
    Joint Tension
AI Thread Summary
The discussion focuses on solving a problem related to joint loading in tension and calculating the cross-sectional areas (CSAs) of various materials. The original poster is struggling to compute the correct CSAs and is advised to reference textbooks for equations related to stress calculations. Key corrections are provided regarding the CSAs of steel, timber, and brass, emphasizing the need for accurate measurements and unit notation. Participants stress the importance of calculating applied stress by dividing force by area and comparing it to material strength to determine failure points. The conversation highlights the necessity of showing work and understanding each step in the problem-solving process.
elephunk
Messages
22
Reaction score
0

Homework Statement



Stuck on this for quite some time.

http://img685.imageshack.us/img685/1387/22580211.png

Homework Equations


The Attempt at a Solution



I've drawn the component parts in question. Don't know where to even begin to find this solution (dont have my scanner here too). I am assuming I need to work out the CSAs of all the materials then move on from there? Need some assistance.

Thanks,
 
Last edited by a moderator:
Physics news on Phys.org
elephunk: Cross-sectional areas are one thing you need. Read a few pages in your textbook to find out how to compute the different types of stress. You must list relevant equations yourself, and show your work; and then someone might check your math.
 
Can you suggest two textbooks I can find this in? I've got technology of engineering materials and mechanical engineering principles and they don't appear to go in depth with stress.This is unlike anything I've done before and I've been searching for the information for days.

I've calculated the CSAs.

Steel CSA = 0.1mm^2
Timber CSA = 0.3mm^2

Thanks
 
elephunk: Your cross-sectional areas are currently incorrect. Try again. Applied stress in this problem is force divided by area. Compare that stress to the given material strength by dividing the applied stress by material strength, which is called stress level, R. The highest stress level governs (fails first). Also, per the international standard (ISO 31-0), always leave a space between a numeric value and its following unit symbol. E.g., 20 mm, not 20mm. Also, N/mm^2 is called MPa. Always use the correct unit symbol (MPa in this case), if a derived unit has a special name.
 
1. You need to be clear about the distinct meanings of s t and tau
2. The end distance given has a clue to another failure mode
 
Steel = 20x5 - (5x5)= 75 mm^2

timber = 20x15-15x5= 270 mm^2

brass = pi*D^2/4=19.625 mm^2

Those are the CSAs. So from then on what do I do with the tmax and smax values. I didn't quite understand what you mean?

This is so confusing for me sorry.
 
Your cross-sectional areas are incorrect. The diameter of the rivet is 10 mm. Try again. After that, compute the stress on the cross-sectional areas. The third sentence of post 4 tells you how to do that. You must list relevant equations yourself, and show your work. We are not allowed to give you the equations nor do your school assignment for you on this site. If you do not understand a particular sentence, explain exactly which part of the sentence or words you do not understand, and explain why you do not understand the words.
 
Back
Top