Loaded beam in compression? (buckles?)

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    Beam Compression
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SUMMARY

The discussion focuses on calculating the deflection of a beam subjected to both a central transverse load and an axial compressive force. It is established that the total deflection is the sum of the deflection due to the transverse load and the additional deflection caused by the axial load's eccentric moment. The maximum stress occurs at the midpoint of the beam and is determined by combining bending stress from the transverse load, axial stress from the compressive load, and additional stresses due to deflection. The critical buckling load must be considered to ensure the beam does not buckle under the axial force.

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  • Understanding of beam mechanics and deflection principles
  • Knowledge of axial load effects on structural elements
  • Familiarity with bending stress calculations (M = HL/4)
  • Concept of critical buckling load in structural analysis
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  • Research "Euler's Buckling Theory" for critical load calculations
  • Study "Beam Deflection Formulas" for various loading conditions
  • Explore "Second Order Effects in Structural Analysis" for advanced stress considerations
  • Learn about "Finite Element Analysis (FEA)" for complex beam behavior simulations
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Structural engineers, civil engineering students, and professionals involved in beam design and analysis will benefit from this discussion.

aortucre
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Hey guys, I know this is a simple question but I'm not really sure how to do it.

Let's say we have a beam supported by two pins at both extremes.
There is a central load on the beam, so it will deflect in the direction of the load.
But we also have an axial force compressing the beam.

My question is how do we calculate the beam's deflection? Do we have to add the deflection due to the transverse load and the deflection due to buckling?

Also, how would we find the maximum stress?

Thanks in advance for any help!
 
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The beam will not buckle if the axial load is below its critical value for buckling. The max stress would be at mid point and at the outer compression fibers and be equal to the bending stress from the transverse load H (bending moment M = HL/4 and bending stress = Mc/I ) plus the compressive stress from the axial load P, (axial stress = P/A), plus the bending moment stress from the axial load P, P(d), where d is the deflection under the transverse load, plus second order stresses from the additional deflection. These latter 2 stresses can sometimes be ignored if P or d is small enough. Beam deflection would be the sum of the deflection due to the transverse load plus the additional deflection due to the eccentric moment caused by the axial load.
 

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