Stiffness of column when fixed versus pin fixed

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Column stiffness is determined by the boundary conditions at the joints, with fixed-fixed columns exhibiting a stiffness of 12EI/L^3, while pin-fixed columns have a stiffness of 3EI/L^3. This distinction arises from the deflection characteristics of beams under lateral loads, where fixed-fixed columns resist rotation and translation, and pin-fixed columns allow for rotation at one end. The stiffness values are derived from the inverse of deflection formulas for beams subjected to point loads at the joints. Understanding these principles is crucial for analyzing structural behavior during lateral loads, such as earthquakes. The discussion emphasizes the importance of recognizing the differences in stiffness based on joint conditions in structural engineering.
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Guys when i study earthquake , they told me that the column stiffness is 12EI/L3 if column is fixed -fixed and 3EI/L3 if column is pin -fixed, so how they get this, i try to study stiffness Matrix and it gives you big matrix for frames not Only one factor like 12EI/L3
please explain
 
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They are not talking about the stiffness of the joints, just the stiffness of the member framing into the joint with a lateral load is applied at the joint. If both ends are fixed at the joints (translation but no relative rotation), K = 12EI/L^3, which is the inverse of its end deflection for a fixed-guided beam subject to point load at the joint, and if it's fixed pinned, then K = 3EI/L^3, the inverse of the deflection of a cantilever with a point load at joint
 


PhanthomJay said:
They are not talking about the stiffness of the joints, just the stiffness of the member framing into the joint with a lateral load is applied at the joint. If both ends are fixed at the joints (translation but no relative rotation), K = 12EI/L^3, which is the inverse of its end deflection for a fixed-guided beam subject to point load at the joint, and if it's fixed pinned, then K = 3EI/L^3, the inverse of the deflection of a cantilever with a point load at joint

Thank you very much. i didnt get it ,could uou provide me with something to read , in order to understand it.Please
 


What do you mean by the inverse of the deflection of a cantilever with a point load at joint?? and how it is equivalent please expalin
 


The deflection of a cantilever with a point load F at the free end is FL^3/3EI. It's stiffness, K, or spring constant if you will, per Hooke's Law F=kx, is

F=kx

k = F/x
k = F/(FL^3/3EI)
k = 3EI/L^3
which is the inverse of the deflection under a unit load.
You are asking why, I think, you use the cantilever stiffness for a fixed pinned column in a frame with a load applied at the joint. That's because the joint translates, and the deflected sahpe is equivalent to the cantilever's deflected shape. For the fixed-fixed case with joint translation, the stiffness is equivalent to that of a beam fixed at one end and free to translate but not rotate at the other, in which case K = 12EI/L^3, which youcan find in beam tables.
 
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