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A Rod Stretched by Its Own Weight

Irodov 1.298DifficultyDifficulty 2 of 5UniquenessUniqueness 2 of 5

Problem Irodov 1.298

A copper rod of length ll hangs vertically, fixed to the ceiling at its upper end, and stretches under its own weight. Find:

  1. (a)

    the elongation Δl\Delta l this self-weight produces;

  2. (b)

    the resulting fractional change in the rod’s volume, ΔV/V\Delta V/V.

The rod of length l hanging under its own weight from its fixed upper end.

The rod of length ll hanging under its own weight from its fixed upper end.

Given
  • copper rod of length ll, fixed at one end
Find
(a) Δl\Delta l, (b) ΔV/V\Delta V/V

Solution

Step 1The tension at a cross-section
An element dx at distance x below the fixed end carries the weight of the length (l-x) still hanging beneath it.

An element dxdx at distance xx below the fixed end carries the weight of the length (l−x)(l-x) still hanging beneath it.

Let AA be the cross-sectional area and ρ\rho the density of copper. Measure xx from the fixed (upper) end, 0≤x≤l0\le x\le l. The cross-section at xx carries the weight of everything hanging below it, a length (l−x)(l-x):

T(x)=ρAg (l−x).(1) T(x) = \rho A g\,(l-x). \tag{1}
Step 2Elongation, by integrating the local strain

Each element’s local strain is T(x)/(EA)T(x)/(EA) with TT from (1), and the total elongation sums this over the rod:

Δl=∫0lT(x)EA dx=ρgE∫0l(l−x) dx=ρgE[lx−x22]0l(2) \Delta l = \int_0^l \frac{T(x)}{EA}\,dx = \frac{\rho g}{E}\int_0^l (l-x)\,dx = \frac{\rho g}{E}\left[lx-\frac{x^2}{2}\right]_0^l \tag{2}
Δl=12ρgl2E\Delta l = \frac{1}{2}\frac{\rho g l^2}{E}
(3)
Step 3The volume change, part (b)

A rod element under axial strain ε(x)=T(x)/(EA)\varepsilon(x) = T(x)/(EA) also contracts sideways by Poisson’s ratio μ\mu: the two transverse strains are each −με(x)-\mu\varepsilon(x). To first order, the local fractional volume change of that element is the sum of all three strains,

dVdV0=ε(x)−2μ ε(x)=(1−2μ) ε(x).\frac{dV}{dV_0} = \varepsilon(x) - 2\mu\,\varepsilon(x) = (1-2\mu)\,\varepsilon(x).

Since dV0=A dxdV_0 = A\,dx, the total volume change is

ΔV=∫0lA(1−2μ)ε(x) dx=A(1−2μ)∫0lε(x) dx=A(1−2μ) Δl,\Delta V = \int_0^l A(1-2\mu)\varepsilon(x)\,dx = A(1-2\mu)\int_0^l \varepsilon(x)\,dx = A(1-2\mu)\,\Delta l,

using the same integral (2) that produced Δl\Delta l. Dividing by V=AlV=Al gives the relative volume change.

ΔVV=(1−2μ)Δll\frac{\Delta V}{V} = (1-2\mu)\frac{\Delta l}{l}
(4)
Check

For an incompressible material, μ=1/2\mu=1/2, the formula gives ΔV/V=0\Delta V/V=0: stretching such a material changes its shape but never its volume, which is the defining property of μ=1/2\mu=1/2.

Remark

The relation ΔV/V=(1−2μ) Δl/l\Delta V/V=(1-2\mu)\,\Delta l/l never used gravity, length, or Young’s modulus directly, only the fractional stretch Δl/l\Delta l/l itself. It therefore holds for any axial strain, however produced, self-weight here, a hanging mass elsewhere, or a testing machine’s grip: two rods of the same material carrying the same fractional elongation always carry the same fractional volume change, regardless of what stretched them.