Each of the segment of this composite bar is subjected to axial pull P =150 kN.
Axial Stress in the middle portion \(\sigma\)2 = Axial pull/Area = 150 × 103 /[(\(\pi\)/4).(d22)]
\(\therefore\) d2 = 39.1 mm
Since stress is limited to 125 N/mm2 , in the middle portion
125 = 150 × 103 /[(\(\pi\)/4).(d22 )]
Diameter of middle portion
d2 = 39.1mm
(ii) Stress in the end portions, \(\sigma\)1 = \(\sigma\)3
= 150 × 103 /[(\(\pi\)/4).(502 )] = 76.43 N/m2
Total change in length of the bar,
= change in length of end portions + change in length of mid portion
δL = δL1 + δL2 + δL3
= \(\sigma\)1L1/E + \(\sigma\)2L2/E + \(\sigma\)3L3/E; Since E is same for all portions
= \(\sigma\)1(L1 + L3)/E + \(\sigma\)2L2/E
L1 + L3 = 300 – L2