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Thin closed ring under diametral compression

Short answer

By Castigliano’s theorem, bending moments at load points and at 90° are 0.318PR (47.7 kN·mm) and 0.182PR (27.3 kN·mm). Maximum bending stress is 79.6 MPa at the load points. The loaded diameter decreases by 0.70 mm.

A thin circular ring of mean radius 150 mm has a rectangular section 25 mm wide (parallel to the axis) and 12 mm thick (radial). It is compressed by two equal and opposite forces of 1 kN acting along a diameter. Using Castigliano's theorem determine the bending moments at the load points and at the section at 90∘90^\circ to the load line, the maximum bending stress, and the decrease in the loaded diameter. Take E=200E = 200 GPa. Neglect the effect of axial and shear forces.

Data

R=150R = 150 mm, P=1000P = 1000 N, b=25b = 25 mm, t=12t = 12 mm, E=200×103E = 200\times10^3 MPa.

I=bt312=25×12312=3600 mm4I = \frac{bt^3}{12} = \frac{25\times12^3}{12} = 3600\ \text{mm}^4

Statically indeterminate moment

The ring is symmetric about both diameters. Cut it at the horizontal section: by symmetry the shear is zero, the normal force is P/2P/2 (compression) and the moment M0M_0 is unknown. The slope of this section does not change, so ∂U/∂M0=0\partial U/\partial M_0 = 0.

          P
          |
        .-v-.
      /       \
  M0 |-- ring --| M0     (cut sections with P/2 each)
      \       /
        '-^-'
          |
          P

For a section at angle θ\theta from the horizontal cut (towards the load):

Mθ=M0−P2R(1−cos⁡θ),∂Mθ∂M0=1M_\theta = M_0 - \frac{P}{2}R(1 - \cos\theta),\qquad \frac{\partial M_\theta}{\partial M_0} = 1 ∂U∂M0=4REI∫0π/2[M0−PR2(1−cos⁡θ)]dθ=0M0 π2=PR2(π2−1)M0=PR(12−1π)=0.1817 PR\begin{aligned} \frac{\partial U}{\partial M_0} &= \frac{4R}{EI}\int_0^{\pi/2}\left[M_0 - \frac{PR}{2}(1-\cos\theta)\right]d\theta = 0 \\ M_0\,\frac{\pi}{2} &= \frac{PR}{2}\left(\frac{\pi}{2} - 1\right) \\ M_0 &= PR\left(\frac12 - \frac1\pi\right) = 0.1817\,PR \end{aligned}

Bending moments

  • At the horizontal section (θ=0\theta = 0, 90∘90^\circ from the load): M0=0.1817×1000×150=27254M_0 = 0.1817\times1000\times150 = 27254 N mm, tension on the outer surface.
  • At the load point (θ=π/2\theta = \pi/2): M=M0−PR/2=−PR/πM = M_0 - PR/2 = -PR/\pi, magnitude 0.3183×1000×150=477460.3183\times1000\times150 = 47746 N mm, tension on the inner surface (opposite sign to M0M_0).

More simply, Mθ=PR(cos⁡θ2−1π)M_\theta = PR\left(\dfrac{\cos\theta}{2} - \dfrac1\pi\right).

Maximum bending stress

The maximum moment is at the load points:

σmax=McI=47746×63600=79.6 MPa\sigma_{max} = \frac{M c}{I} = \frac{47746\times6}{3600} = 79.6\ \text{MPa}

At the horizontal section: σ=27254×6/3600=45.4\sigma = 27254\times6/3600 = 45.4 MPa. (The direct stress P/2A=500/300=1.7P/2A = 500/300 = 1.7 MPa is small and is neglected, as stated.)

Change in loaded diameter

δV=∂U∂P=4REI∫0π/2Mθ ∂Mθ∂P dθ=4PR3EI∫0π/2(cos⁡θ2−1π)2dθ=4PR3EI(π16−12π)=PR3EI(π4−2π)=0.1488 PR3EI\begin{aligned} \delta_V &= \frac{\partial U}{\partial P} = \frac{4R}{EI}\int_0^{\pi/2} M_\theta\,\frac{\partial M_\theta}{\partial P}\,d\theta = \frac{4PR^3}{EI}\int_0^{\pi/2}\left(\frac{\cos\theta}{2} - \frac1\pi\right)^2 d\theta \\ &= \frac{4PR^3}{EI}\left(\frac{\pi}{16} - \frac{1}{2\pi}\right) = \frac{PR^3}{EI}\left(\frac\pi4 - \frac2\pi\right) = 0.1488\,\frac{PR^3}{EI} \end{aligned} δV=0.1488×1000×1503200×103×3600=0.697 mm\delta_V = 0.1488\times\frac{1000\times150^3}{200\times10^3\times3600} = 0.697\ \text{mm}

The loaded diameter decreases by this amount, and the horizontal diameter increases by about 0.137 PR3/EI0.137\,PR^3/EI.

Answer: Mload=47746M_{load} = 47746 N mm (0.318 PRPR), M90∘=27254M_{90^\circ} = 27254 N mm (0.182 PRPR, opposite sign), σmax=79.6\sigma_{max} = 79.6 MPa, decrease in loaded diameter =0.70= 0.70 mm.

✓ Answer checked by Claude Sonnet 5.5

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