A composite bar consists of an aluminum section rigidly fastened between a bronze section and a steel section as shown in Fig. 1-8a. Axial loads are applied at the positions indicated. Determine the stress in each section.
Figure 1.8a
Solution:
We must first determine the axial load in each section to calculate the stresses. The free-body diagrams have been drawn by isolating the portion of the bar lying to the left of imaginary cutting planes. Identical results would be obtained if portions lying to the right of the cutting planes had been considered.
Solve for the internal axial load of the bronze
The free-body diagram of the bronze section
∑ F x = 0 → − 4000 lb + P b r = 0 P b r = 4000 lb (tension) \begin{align*}
\sum_{}^{}F_x & = 0 \to \\
-4000\ \text{lb}+P_{br} & = 0 \\
P_{br} & = 4000 \ \text{lb} \ \text{(tension)}
\end{align*} ∑ F x − 4000 lb + P b r P b r = 0 → = 0 = 4000 lb (tension)
Solve for the internal axial load of the aluminum
The free-body diagram of the aluminum section
∑ F x = 0 − 4000 lb + 9000 lb − P a l = 0 P a l = 5000 lb (Compression) \begin{align*}
\sum_{}^{}F_x & = 0 \\
-4000 \ \text{lb} + 9000 \ \text{lb} - P_{al} & = 0 \\
P_{al} & = 5000 \ \text{lb} \ \text{(Compression)}
\end{align*} ∑ F x − 4000 lb + 9000 lb − P a l P a l = 0 = 0 = 5000 lb (Compression)
Solve for the internal axial load of the aluminum
The free-body diagram of the steel section
∑ F x = 0 − 4000 lb + 9000 lb + 2000 lb − P s t = 0 P s t = 7000 lb (Compression) \begin{align*}
\sum_{}^{}F_x & = 0 \\
-4000\ \text{lb} + 9000 \ \text{lb} + 2000\ \text{lb} - P_{st} & =0 \\
P_{st} & = 7000 \ \text{lb} \ \text{(Compression)}
\end{align*} ∑ F x − 4000 lb + 9000 lb + 2000 lb − P s t P s t = 0 = 0 = 7000 lb (Compression)
We can now solve the stresses in each section.
For the bronze
σ b r = P b r A b r = 4000 lb 1.2 in 2 = 3330 psi (Tension) ( Answer ) \begin{align*}
\sigma_{br} & = \frac{P_{br}}{A_{br}} \\
& = \frac{4000\ \text{lb}}{1.2 \ \text{in}^2} \\
& = 3330 \ \text{psi}\ \text{(Tension)} \ \qquad \ \color{DarkOrange} \left( \text{Answer} \right)
\end{align*} σ b r = A b r P b r = 1.2 in 2 4000 lb = 3330 psi (Tension) ( Answer )
For the aluminum
σ a l = P b r A a l = 5000 lb 1.8 in 2 = 2780 psi (Compression) ( Answer ) \begin{align*}
\sigma_{al} & = \frac{P_{br}}{A_{al}} \\
& = \frac{5000\ \text{lb}}{1.8 \ \text{in}^2} \\
& = 2780 \ \text{psi}\ \text{(Compression)} \ \qquad \ \color{DarkOrange} \left( \text{Answer} \right)
\end{align*} σ a l = A a l P b r = 1.8 in 2 5000 lb = 2780 psi (Compression) ( Answer )
For the steel
σ s t = P s t A s t = 7000 lb 1.6 in 2 = 4380 psi (Compression) ( Answer ) \begin{align*}
\sigma_{st} & = \frac{P_{st}}{A_{st}} \\
& = \frac{7000\ \text{lb}}{1.6 \ \text{in}^2} \\
& = 4380\ \text{psi}\ \text{(Compression)} \ \qquad \ \color{DarkOrange} \left( \text{Answer} \right)
\end{align*} σ s t = A s t P s t = 1.6 in 2 7000 lb = 4380 psi (Compression) ( Answer )
You must be logged in to post a comment.