How Is Stress Calculated in a Bar Using Transposed Formulas?

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Stress in a bar is calculated using transposed formulas that incorporate thermal expansion coefficients, lengths, temperature changes, and stress-strain relationships. The highlighted line 1/E(σ1L1+σ2L2)=0 arises from simplifying the expression when assuming uniform material properties (E1=E2). This simplification shows that the stress terms can be factored out with respect to the modulus of elasticity. The discussion clarifies that the equation is valid under the condition that E1 and E2 are equal. Understanding these relationships is crucial for accurate stress calculations in structural analysis.
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Need to find stress in a bar

(α1L1ΔT1+x1)+(α2L2ΔT2+x2)=0

(α1L1ΔT1+ε1L1)+(α2L2ΔT2+ε2L2)=0

(α1L1ΔT1+σ1/E1*L)+(α2L2ΔT2+σ2/E2*L)=0

(α1L1ΔT1+α2L2ΔT2)+σ1/E1*L1+σ2/E2*L2=0

αΔT(L1+L2)+1/E(σ1L1+σ2L2)=0

I can work out most of this formula but i don't understand how we got the highlighted line 1/E(σ1L1+σ2L2)=0
 
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anthonyk2013 said:
i don't understand how we got the highlighted line 1/E(σ1L1+σ2L2)=0
You don't mean the '=0' there, right?
I presume it should be (σ1/E1)*L1+(σ2/E2)*L2 and (1/E)(σ1L1+σ2L2), which are the same if E=E1=E2. With no context, I cannot tell whether E1=E2.
 
No=0 fine. It 1/E where did that come from.
 
anthonyk2013 said:
No=0 fine. It 1/E where did that come from.
You have (σ1/E1)*L1+(σ2/E2)*L2. If E1=E2=E then that reduces to (σ1/E)*L1+(σ2/E)*L2 = (1/E)(σ1)*L1+(1/E)(σ2)*L2 = (1/E)(σ1L1+σ2L2).
 
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