The solid cylindrical rod BC of length L = 24 in. is attached to the rigid lever AB of length a = 15 in. and to the support at C. Design specifications require that the displacement of A not exceed 1 in. when a 100-lb force P is applied at A. For the material indicated, determine the required diameter of the rod.
Steel: τall = 15 ksi, G = 11.2 × 106 psi.
Fig. P10.39

Calculate the Torque applied on the shaft due to the force applied at \(A\).
$$ T=P \times a $$
Here, \(P\) is the applied load, \(a\) is distance of line of action of force from axis of shaft.
Substitute \(100 \mathrm{lb}\) for \(P\) and 15 in for \(a\).
$$ \begin{aligned} T &=(100 \mathrm{lb})(15 \mathrm{in} .) \\ &=1500 \mathrm{lb} \cdot \mathrm{in} . \end{aligned} $$
Write the equation for the allowable shear stress of a solid shaft.
$$ \tau_{\mathrm{all}}=\frac{16 T}{\pi d^{3}} $$
$$ d=\left(\frac{16 T}{\pi \tau_{\mathrm{all}}}\right)^{\frac{1}{3}} $$
Here, \(\tau_{\text {all }}\) is the allowable shear stress.
Substitute \(1500 \mathrm{lb} \cdot \mathrm{in}\). for \(T\) and \(15 \times 10^{3} \mathrm{lb} / \mathrm{in} .{ }^{2}\) for \(\tau_{\mathrm{all}}\)
$$ \begin{aligned} d &=\left[\frac{16(1500 \mathrm{lb} \cdot \mathrm{in} .)}{\pi\left(15 \times 10^{3} \mathrm{lb} / \mathrm{in} .^{2}\right)}\right]^{\frac{1}{3}} \\ &=0.8 \mathrm{in} . \end{aligned} $$
Calculate the maximum allowable angular twist.
$$ \phi_{\text {all }}=\frac{s_{\max }}{\mathrm{a}} $$
Here, \(s_{\max }\) is the maximum allowable displacement of point \(A\) and \(a\) is the distance of the line of action of force from the axis of the shaft.
Substitute \(0.1\) in. for \(s_{\max }\) and 15 in. for \(a\).
$$ \begin{aligned} \phi_{\text {all }} &=\frac{1 \mathrm{in} .}{15 \mathrm{in} .} \\ &=0.067 \mathrm{rad} \end{aligned} $$
This angular twist is same for both \(B\) and point \(A\).
Write the equation for the angular of twist in the shaft.
$$ \begin{array}{l} \phi=\frac{T L}{J G} \\ \phi_{\text {all }}=\frac{T L}{\frac{\pi}{32} d^{4} G} \\ d=\left(\frac{32 T L}{\pi G \phi_{\text {all }}}\right)^{\frac{1}{4}} \end{array} $$
Here, \(G\) is the rigidity modulus of the shaft.
Substitute \(11.2 \times 10^{6} \mathrm{lb} / \mathrm{in} .{ }^{2}\) for \(G, 1500 \mathrm{lb} \cdot \mathrm{in} .\) for \(T, 15 \times 10^{3} \mathrm{lb} / \mathrm{in} .{ }^{2}\) for \(\tau_{\mathrm{all}}, 24 \mathrm{in} .\) for \(L\), and
\(0.067 \mathrm{rad}\) for \(\phi_{\text {all }}\).
$$ d=\left[\frac{32(1500 \mathrm{lb} \cdot \mathrm{in} .)(24 \mathrm{in} .)}{\pi\left(11.2 \times 10^{6} \mathrm{lb} / \mathrm{in}^{2}\right)(0.067)}\right]^{1 / 4} $$
\(=0.837\) in.
Consider the two values obtained, the higher value holds the key for the design condition considering the minimum required diameter.
Hence, the minimum diameter of the shaft is \(0.837\) in.