Understanding strain in stiffness matrix

AI Thread Summary
The discussion focuses on understanding strain in a stiffness matrix for a rod with two nodes under axial forces. Strain is defined as the change in length per unit length, expressed as e = (u1 - u2)/l or e = (u2 - u1)/l, depending on the reference point. The participants clarify that if one node is fixed, the strain at the other node can be calculated based on its displacement relative to the fixed point. The sign convention for strain is emphasized, indicating that positive strain occurs with rightward displacement and negative strain with leftward displacement. Overall, the key takeaway is the importance of consistent sign conventions and understanding the relationship between displacement and strain in different loading conditions.
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Homework Statement



node1 node2
O---------------------------------------O

a rod with 2 nodes:
x1=axial force at node1
x2=axial force at node2
u1,axial deflection at node1
u2,axial deflection at node2
l=elements length
E=young's modulus
A=cross sectional area of rod element
e=strain

I don't understand why at node 1:

e=(u1-u2)/l

and from equilibrium considerations at node 2:

e=(u2-u1)/l

Homework Equations



The Attempt at a Solution



From what i understand, if one end is fixed say node2 then strain at node 1 will be:
u1/l

and if node1 is fixed then strain at node2:
u2/l

at node 1, if i assume that the direction of force/displacement from node1 to node2 is positive isn't that supposed to be negative because of compression?

and i don't understand how u1-u2 or u2-u1 works? Can somebody explain it to me and give me an example?
 
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Hello xpp8 welcome to PF

strain is defined as deflection per unit length, i.e. \epsilon = \frac{\delta}{L_0} where \delta = L' - L_0 i.e. the change in length of the member due to the axial force. where L_0 is the original length and L' is the new length.

\epsilon is important because a large deflection for a small length can easily allow the member the exceed the elastic limit or \sigma_{y} and become plastic or permanently deformed.

Try it...stretch a small rubber band -of length a fixed at one end for some large \delta just before it pops, it can probably remain elastic. then stretch an even smaller rubber band say of length \frac{1}{5}a do you think the smaller of the two can withstand the same \delta? no

This is characterized by strain \epsilon = \frac{\delta}{L_0}
 
Hi djeitnstine,

How do i relate (L'-Lo)/Lo with e=(u1-u2)/l ?

if in equilibrium(tension/compression with X1=-X2, E and A are constant) U1 and U2 will be the same in magnitude but different in direction, what about in non-equilibrium(X1 not equal to -X2 ) state where the direction and magnitude might be different. How do i visualize such elastic behaviour?
 
Seems like a strange sign convention. Let's assume node 1 is fixed, and node 2 is free to move, and the member is in tension and in equilibrium. Then the displacement u1 of node 1 is 0, the displacement of node 2 is u2 to the right, and the strain at either node node is u2/l. If node 2 is fixed and node 1 is free, then u2 is 0 and the displacement of node 1 is u1 to the left, and the strain at either node is u1/l. If both nodes 1 and 2 are both free to move, let's say equally from the mid point, then u1 = u2, and the displacement of node 1 is u1 to the left, the displacemnt of node 2 is u2 to the right, and the strain is (u1 + u2)/l at either node. In all cases, the strain is the same. Your formula seems to choose a sign convention that calls strain positive if the deformation is to the right, and negative if it is to the left. It's all in the plus and minus sign.
 
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