We are given two solid shafts, P and Q, transmitting the same torque ($T$). They are made of the same material.
The cross-section is circular. Let $r_P$ and $r_Q$ be the radii of shafts P and Q, respectively.
The area of a circular cross-section is given by $A = \pi r^2$. Therefore:
For shaft P: $A_P = \pi r_P^2 = A$
For shaft Q: $A_Q = \pi r_Q^2 = 4A$
Comparing the areas:
$\pi r_Q^2 = 4 (\pi r_P^2)$
$r_Q^2 = 4 r_P^2$
$r_Q = 2 r_P$
This means the radius of shaft Q is twice the radius of shaft P.
The polar moment of inertia ($J$) for a solid circular shaft is given by $J = \frac{\pi r^4}{2}$.
For shaft P: $J_P = \frac{\pi r_P^4}{2}$
For shaft Q: $J_Q = \frac{\pi r_Q^4}{2}$
Substituting $r_Q = 2 r_P$ into the expression for $J_Q$:
$J_Q = \frac{\pi (2 r_P)^4}{2} = \frac{\pi (16 r_P^4)}{2} = 16 \left( \frac{\pi r_P^4}{2} \right)$
$J_Q = 16 J_P$
The polar moment of inertia of shaft Q is 16 times that of shaft P.
The maximum torsional shear stress ($\tau$) in a solid circular shaft is related to the applied torque ($T$), the outer radius ($r$), and the polar moment of inertia ($J$) by the formula:
$\tau = \frac{T r}{J}$
For shaft P, the maximum shear stress is given:
$\tau_P = \frac{T r_P}{J_P} = 160 \text{ MPa}$
For shaft Q, the maximum shear stress is:
$\tau_Q = \frac{T r_Q}{J_Q}$
Substitute $r_Q = 2 r_P$ and $J_Q = 16 J_P$ into the equation for $\tau_Q$:
$\tau_Q = \frac{T (2 r_P)}{16 J_P} = \frac{2}{16} \frac{T r_P}{J_P} = \frac{1}{8} \frac{T r_P}{J_P}$
Since $\tau_P = \frac{T r_P}{J_P}$, we can write:
$\tau_Q = \frac{1}{8} \tau_P$
Now, substitute the value of $\tau_P$:
$\tau_Q = \frac{1}{8} \times 160 \text{ MPa}$
$\tau_Q = 20 \text{ MPa}$
The maximum torsional shear stress developed in shaft Q is 20 MPa.
Both the numerator and the denominator of $\frac{3}{4}$ are increased by a positive integer, x, and those of $\frac{15}{17}$ are decreased by the same integer. This operation results in the same value for both the fractions.
What is the value of x?
| Metal | Pilling-Bedworth Ratio |
| Li | 0.57 |
| Ce | 1.16 |
| Ta | 2.33 |
| W | 3.40 |