1. | \(B_1\) | 2. | \(2B_1\) |
3. | \( \dfrac {B_1}{2}\) | 4. | \(\dfrac {B_1}{\sqrt 2}\) |
1. | 2. | ||
3. | 4. |
1. | no stress. | 2. | compressive stress. |
3. | tensile stress. | 4. | shear stress. |
1. | \(\dfrac{3 M g l}{A Y}\) | 2. | \(\dfrac{2 M g l}{A Y}\) |
3. | \(\dfrac{3 M g l}{2 A Y}\) | 4. | \(\dfrac{M g l}{A Y}\) |
1. | tensile, \(\dfrac{F}{3A}\) |
2. | compressive, \(\dfrac{F}{3A}\) |
3. | tensile, \(\dfrac{2F}{3A}\) |
4. | compressive, \(\dfrac{2F}{3A}\) |
Two wires of identical dimensions but of different materials having Young's moduli \(Y_1, Y_2\) are joined end to end. When the first wire is under a tension \(T,\) it elongates by \(x_1\) while the second wire elongates by \(x_2\) under the same tension \(T.\) The elongation of the composite wire when it is under tension \(T\) is:
1. | \(x_1+x_2\) | 2. | \(\dfrac{Y_1x_1+Y_2x_2}{Y_1+Y_2}\) |
3. | \(\dfrac{x_1+x_2}{2}\) | 4. | \(\dfrac{Y_1x_2+Y_2x_1}{Y_1+Y_2}\) |