Elasticity — Question 5

Section 12-6 · Physics pages 1880–1881

Question 5 A hanging rod carries a nonuniform stress from its own weight A uniform vertical rod hangs from its top under its own weight. Its length is L = 100 m, density ρ = 8000 kg/m3 and modulus E = 200 GPa. Use g = 10 m/s2 and constant area A; neglect geometric changes. x L The tension at a cut supports only the material below it. (a) Using x measured downward from the top, find the tension profile and total elongation. (b) Find the largest stress and explain why doubling area does not change the self-weight elongation.
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Question 5 - Solution A hanging rod carries a nonuniform stress from its own weight x L (a) Derivation and calculation A section at depth x supports the rod below it: N(x) = ρAg(L −x) , σ(x) = ρg(L −x). Integrating strain over length gives δ = ∫L 0 N(x) EA dx = ρgL2 2E . δ = 8000(10)(100)2 2(200 × 109) = .00200 m = 2.00 mm . (b) Result and interpretation Maximum stress occurs at the top: σmax = ρgL = 8000(10)(100) = 8.00 MPa . Doubling A doubles both N(x) and EA: 2N(x) E(2A) = N(x) EA . The strain profile and total self-weight extension therefore remain unchanged. Physical check Tension decreases linearly from the full rod weight at the top to zero at the free end.

Question 5

A hanging rod carries a nonuniform stress from its own weight

A uniform vertical rod hangs from its top under its own weight. Its length is L=100mL=100\,\mathrm m, density ρ=8000kg/m3\rho=8000\,\mathrm{kg/m^3} and modulus E=200GPaE=200\,\mathrm{GPa}. Use g=10m/s2g=10\,\mathrm{m/s^2} and constant area AA; neglect geometric changes.

Diagram shown in the original SVG worksheet.

  1. Using xx measured downward from the top, find the tension profile and total elongation.

  2. Find the largest stress and explain why doubling area does not change the self-weight elongation.

Question 5 - Solution

A hanging rod carries a nonuniform stress from its own weight

Diagram shown in the original SVG worksheet.

(a) Derivation and calculation

A section at depth xx supports the rod below it: N(x)=ρAg(L−x),σ(x)=ρg(L−x).\boxed{N(x)=\rho Ag(L-x)},\qquad\sigma(x)=\rho g(L-x). Integrating strain over length gives δ=∫0LN(x)EAdx=ρgL22E.\delta=\int_0^L\frac{N(x)}{EA}\,dx=\frac{\rho gL^2}{2E}. δ=8000(10)(100)22(200×109)=.00200m=2.00mm.\boxed{\delta=\frac{8000(10)(100)^2}{2(200\times10^9)}=.00200\ \mathrm m=2.00\ \mathrm{mm}}.

(b) Result and interpretation

Maximum stress occurs at the top: σmax=ρgL=8000(10)(100)=8.00MPa.\boxed{\sigma_{\max}=\rho gL=8000(10)(100)=8.00\ \mathrm{MPa}}. Doubling AA doubles both N(x)N(x) and EAEA: 2N(x)E(2A)=N(x)EA.\frac{2N(x)}{E(2A)}=\frac{N(x)}{EA}. The strain profile and total self-weight extension therefore remain unchanged.

Physical check

Tension decreases linearly from the full rod weight at the top to zero at the free end.