SM 143 Deflection of beams

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Last updated 3:25 PM on 3/30/26
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4 Terms

1
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Curvature formula

  • 1/ρ is called curvature. EI is called flexural rigidity.

  • ρ is radius of curvature, M is internal moment, E is young modulus, I is moment of inertia.

  • sign of ρ depends on direction of M: when M is positive, ρ extends above the beam in positive υ direction, and vice versa

<ul><li><p>1/ρ is called curvature. EI is called flexural rigidity.</p></li><li><p>ρ is radius of curvature, M is internal moment, E is young modulus, I is moment of inertia.</p></li><li><p>sign of ρ depends on direction of M: when M is positive, ρ extends above the beam in positive υ direction, and vice versa</p></li></ul><p></p>
2
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Calculus relationships from w(x) to v

From curvature onwards always have 1/EI

clarification: Integral of M(x) = θ/EI + C

<p>From curvature onwards always have 1/EI</p><p>clarification: Integral of M(x) = <span>θ/EI + C</span></p>
3
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Boundary conditions

  • At point force (includes supports) that is not at ends of beam: θ1 = θ2, which can be used to equate slope equations to left and right of boundary

Only θ and y is important for slope and deflection formulas

<ul><li><p>At point force (includes supports) that is not at ends of beam: <strong><span>θ</span><sub><span>1</span></sub><span> = θ</span><sub><span>2</span></sub></strong><span>, which can be used to equate slope equations to left and right of boundary</span></p></li></ul><p><strong><span>Only θ and y is important for slope and deflection formulas</span></strong></p>
4
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Finding Cs

Use boundary conditions and boundary positions.

eg. x = L/4 is boundary position and at that boundary θ1 = θ2. Substitute L/4 into your θ1 & θ2 equations to equate some C values.

eg. at x = 0, y1 = 0, then all x terms get cancelled and C is set to 0.

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