Strength of materials- simple truss problem

AI Thread Summary
The discussion revolves around solving a simple truss problem involving axial stress and elongation of members. The maximum axial stress is set at 25 ksi, leading to a calculated maximum load (Pmax) of 30 kip based on the cross-sectional area of 1.2 in². The user derived the strain (epsilon) as 8.62E-4 and calculated the elongation (delta) for a member length of 4 ft, resulting in 0.0414 in. There is uncertainty about whether this approach is correct, particularly regarding the uniformity of elongation across members and the need to analyze forces in each truss member. Clarification is sought on the direction of load P and whether further calculations are necessary to determine individual member forces.
Jeff231
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Homework Statement



The bars in the truss each have a cross sectional area of 1.2in^2. If the maximum axial stress in any bar is not to exceed 25ksi, determine the maximum magnitude of P of the loads that can be applied to the truss. Determine the elongation of each member.

E=29,000 ksi


4930827627_46098ef021.jpg


Homework Equations



<br /> \sigma = E* \epsilon

\sigma = P/A


\epsilon = \delta / L

Having trouble with Latex, but the top equation should read:
sigma=E*epsilon

the other two equations are stress=force/area and strain=elongation/lenth.

The Attempt at a Solution



I got an answer, but I'm not sure if it's correct and if I'm solving this correctly.

Since I know \sigma=25ksi, and E=29,000 ksi I used \sigma=P/A solving for P, P= \sigmaA=(25ksi)(1.2in^2)=30 kip.

I assumed this to be Pmax.

Using \sigma=E*epsilon I solved for epsilon. epsilon= \sigma/E=25ksi/29000ksi = 8.62E-4.

Then used epsilon=delta/L. Solved for elongation, delta. delta=epsilon*L.

Then I just used plugged in my solved value of epsilon, and then the length of each bar.

Here's an example for AC: delta=epsilon*L=(8.62E-4)(4ft)(12in/1ft)=0.0414in.


I'm not sure if this correct since it would mean every bar that is the same length would have the same elongation. Is this correct? Or do I need to solve the system for the forces and then do something? I'm confused. Thank you for the help.
 
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Axial stress is generated by a force perpendicular to the cross section, what is the direction of P in the diagram ?
 
Can you determine the force in each member of the truss, as a function of P?
 

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