A not-so-standard buckling problem

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The discussion focuses on determining the critical buckling load (PCR) for an L-shaped rigid bar structure supported by linear elastic springs at points A and C. The relationship between rotational stiffness (βR) and translational stiffness (β) is established as βR = 3βL2/2. The critical buckling load is calculated using the formula PCR = (π²EI)/L², where E is Young's modulus, I is the moment of inertia, and L is the length of the bar. The participant suggests using the Euler-Bernoulli beam equation to derive the necessary values for I and subsequently calculate PCR.

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irishmts
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Hey guys, this came up in one of my past papers, and I'm not quite sure where to go with it.

The diagram shows an idealized structure consisting of an L-shaped rigid bar structure supported b linearly elastic springs at A and C. Rotational Stiffness is denoted βR and translational stiffness is denoted β. If βR = 3βL2/2, determine the critical buckling load PCR for the structure




PCR = C2EI/L, where C is a constant which depends on the end characteristics of the bar, E is youngs modulus, I is inertia, and L is the length of the bar.

Given that the Bar is simply supported, that meant that Le was equal to L/2 i though, and by Le = L/sqrt(C), that gave C a value of 1/4




My first though was to try and resolve the forces being applied, so I took moments about the point of maximum deflection, L/2, when a force of P is applied, where P<PCR. But I got lost there, because I can't figure out what the moment due to the stiffnesses would be, since they are a ratio due to the force applied/ deflection, and I don't know what deflection there would be at the point the spring is attached to
 

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the wall.To solve this problem, you will need to use the Euler-Bernoulli beam equation. The equation can be written as PCR = (π2EI)/L2. Since the rotational stiffness is given, you can calculate the value of I by using βR = 3βL2/2. Substituting I into the equation, you can then calculate the value of PCR.
 

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