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Steel rod inside copper tube

Short answer

From strain compatibility, load stresses: σs = 112.3 MPa, σc = 56.2 MPa (both compressive); loads Ps = 79.4 kN, Pc = 70.6 kN; shortening 0.337 mm. For ΔT = 40°C, internal thermal force 13.31 kN, final stresses: σs = –93.5 MPa, σc = –66.8 MPa.

A steel rod 30 mm in diameter is placed concentrically inside a copper tube of 30 mm inside and 50 mm outside diameter. Both are 600 mm long and are loaded through rigid end plates by an axial compressive load of 150 kN. Es = 200 GPa, Ec = 100 GPa. (a) Find the stress in each material, the load carried by each, and the shortening. (b) The temperature then rises by 40 degrees C. Find the final stress in each material. Take alpha for steel = 12 x 10^-6 and for copper = 17 x 10^-6 per degree C.

Section areas

As=π4(30)2=706.9 mm2A_s = \frac{\pi}{4}(30)^2 = 706.9\ \text{mm}^2, Ac=π4(502−302)=1256.6 mm2A_c = \frac{\pi}{4}(50^2 - 30^2) = 1256.6\ \text{mm}^2.

(a) Load sharing

Equilibrium: Ps+Pc=150×103P_s + P_c = 150\times10^3 N. Compatibility (same shortening, same length): εs=εc\varepsilon_s = \varepsilon_c, so

σsEs=σcEc  ⇒  σc=σsEcEs=0.5 σs\frac{\sigma_s}{E_s} = \frac{\sigma_c}{E_c} \;\Rightarrow\; \sigma_c = \sigma_s\frac{E_c}{E_s} = 0.5\,\sigma_s σsAs+σcAc=150000  ⇒  σs (706.9+0.5×1256.6)=150000\sigma_s A_s + \sigma_c A_c = 150000 \;\Rightarrow\; \sigma_s\,(706.9 + 0.5\times1256.6) = 150000 σs=112.3 MPa,σc=56.2 MPa\sigma_s = 112.3\ \text{MPa}, \qquad \sigma_c = 56.2\ \text{MPa} Ps=112.3×706.9=79.4 kN,Pc=56.2×1256.6=70.6 kNP_s = 112.3\times706.9 = 79.4\ \text{kN}, \qquad P_c = 56.2\times1256.6 = 70.6\ \text{kN}

(check: 79.4+70.6=15079.4 + 70.6 = 150 kN)

δ=σsLEs=112.3×600200000=0.337 mm (shortening)\delta = \frac{\sigma_s L}{E_s} = \frac{112.3\times600}{200000} = 0.337\ \text{mm (shortening)}

(b) Temperature rise of 40 degrees C

Copper tends to expand more than steel, but they are held together. Copper is held back (extra compression) and steel is pulled along (extra tension). The internal forces are equal and opposite, PtP_t:

αcΔTL−PtLAcEc=αsΔTL+PtLAsEs\alpha_c\Delta T L - \frac{P_t L}{A_cE_c} = \alpha_s\Delta T L + \frac{P_t L}{A_sE_s} Pt=(αc−αs)ΔT1AcEc+1AsEs=5×10−6×4011256.6×105+1706.9×2×105=13.31 kNP_t = \frac{(\alpha_c - \alpha_s)\Delta T}{\dfrac{1}{A_cE_c} + \dfrac{1}{A_sE_s}} = \frac{5\times10^{-6}\times 40}{\dfrac{1}{1256.6\times10^5} + \dfrac{1}{706.9\times2\times10^5}} = 13.31\ \text{kN}

Thermal stresses: steel =+13310/706.9=+18.8= +13310/706.9 = +18.8 MPa (tension), copper =−13310/1256.6=−10.6= -13310/1256.6 = -10.6 MPa (compression).

Final stresses (add to the load stresses, compression negative):

MaterialLoadThermalFinal
Steel−112.3-112.3+18.8+18.8−93.5-93.5 MPa
Copper−56.2-56.2−10.6-10.6−66.8-66.8 MPa

Check: −93.5×706.9−66.8×1256.6=−150-93.5\times706.9 - 66.8\times1256.6 = -150 kN.

Answer: (a) σs=112.3\sigma_s = 112.3 MPa, σc=56.2\sigma_c = 56.2 MPa (both compressive), Ps=79.4P_s = 79.4 kN, Pc=70.6P_c = 70.6 kN, shortening 0.3370.337 mm; (b) final σs=−93.5\sigma_s = -93.5 MPa, σc=−66.8\sigma_c = -66.8 MPa.

✓ Answer checked by Claude Opus 5.5 (high effort)

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