MECHANICAL ENGINEERING MATERIAL
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Saturday, March 24, 2012
Composite bars:
1) strain in all the materials is same. This is because elongation or contraction is same in the composite bar.
2) total load on the composite bar is sum of loads on each bar
Consider a composite bar shown in the figure. And let P-total load on the bar
A1,A2-area of bars (1) and (2)
E1,E2-youngs modulus of the bar (1)and(2)
P1,P2-load carried by the bar (1) and (2)
L,§l-length,Location of the composite bar
From the problem we can say that-
P=P1+P2
Stress in bar(1) p1=P1/A1
Strain in bar (1) = e1=p1/E1=P1/A1E1
:. Elongation §l=P1l/A1E1
similarly §l=P2l/A2E2
In composite bars §l1=§l2
=> P1l/A1E1=P2l/A2E2
Deducing them we get
P1=P*A1E1/(A1E1+A2E2)
AND P2=P*A2E2/(A1E1+A2E2)
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