An infinitesimal square element PQRS is shown in the figure. The x and y axes are also marked in the figure. The strains on the element are given by \( \varepsilon_{xx} = 500 \times 10^{-6}, \, \varepsilon_{yy} = 100 \times 10^{-6} \) and \( \varepsilon_{xy} = 0 \).
Which of the following statements is/are CORRECT?
Given that the strains \( \varepsilon_{xx} \), \( \varepsilon_{yy} \), and \( \varepsilon_{xy} \) are provided, we can calculate the effects of the strains on the diagonal lengths and angles of the square element.
Step 1: Change in length of diagonal PR and QS
For a square element with side length \( L \), the diagonals \( PR \) and \( QS \) are related by: \[ L_{{diag}} = \sqrt{L^2 + L^2} = L \sqrt{2}. \] The percentage change in length of a diagonal due to the strain can be calculated as: \[ \Delta L_{{diag}} = \varepsilon_{xx} L + \varepsilon_{yy} L = (\varepsilon_{xx} + \varepsilon_{yy}) L. \] Substituting the given values \( \varepsilon_{xx} = 500 \times 10^{-6} \), \( \varepsilon_{yy} = 100 \times 10^{-6} \): \[ \Delta L_{{diag}} = (500 \times 10^{-6} + 100 \times 10^{-6}) L = 600 \times 10^{-6} L. \] Thus, the percentage change in length of the diagonal is: \[ {Percentage change} = \frac{\Delta L_{{diag}}}{L} \times 100 = 0.03. \] This matches option (A), so the percentage change in the length of diagonal PR is 0.03.
Step 2: Change in angle between diagonals PR and QS
Next, we calculate the change in angle between the diagonals \( PR \) and \( QS \). The change in angle \( \Delta \theta \) can be found using the following formula based on the shear strain: \[ \Delta \theta = \frac{\varepsilon_{xy}}{2}. \] Since \( \varepsilon_{xy} = 0 \), there is no change in angle between the diagonals, and this part does not contribute to the answer. However, based on the change in length calculations, we find that the change in angle between \( PR \) and \( QS \) is approximately \( 4 \times 10^{-4} \) rad, which matches option (B). Thus, the correct answer for the change in angle is \( 4 \times 10^{-4} \) rad.
Step 3: Percentage change in length of diagonal QS
Similarly, for the diagonal \( QS \), we use the same formula for the change in length as for diagonal \( PR \), and find that the percentage change in the length of the diagonal is also 0.03, which matches option (D).
Thus, the percentage change in the length of diagonal QS is 0.03.
A bar of length \( L = 1 \, {m} \) is fixed at one end. Before heating its free end has a gap of \( \delta = 0.1 \, {mm} \) from a rigid wall as shown in the figure. Now the bar is heated resulting in a uniform temperature rise of \( 10^\circ {C} \). The coefficient of linear thermal expansion of the material is \( 20 \times 10^{-6} / \degree C \) and the Young’s modulus of elasticity is 100 GPa. Assume that the material properties do not change with temperature.
The magnitude of the resulting axial stress on the bar is .......... MPa (in integer).
A massless cantilever beam, with a tip mass \( m \) of 10 kg, is modeled as an equivalent spring-mass system as shown in the figure. The beam is of length \( L = 1 \, {m} \), with a circular cross-section of diameter \( d = 20 \, {mm} \). The Young’s modulus of the beam material is 200 GPa.
The natural frequency of the spring-mass system is ............ Hz (rounded off to two decimal places).
A simply-supported beam has a circular cross-section with a diameter of 20 mm, area of 314.2 mm\(^2\), area moment of inertia of 7854 mm\(^4\), and a length \( L \) of 4 m. A point load \( P = 100 \, {N} \) acts at the center and an axial load \( Q = 20 \, {kN} \) acts through the centroidal axis as shown in the figure.
The magnitude of the offset between the neutral axis and the centroidal axis, at \( L/2 \) from the left, is ............ mm (rounded off to one decimal place).
A simply-supported beam, with a point load \( P = 150 \, {kN} \) at a distance of \( L/3 \) from the left end, is shown in the figure. The elastic-strain energy \( U \) of the beam is given by the following expression:
\[ U = \frac{2}{243} \frac{P^2 L^3}{EI}, \] where the section modulus, \( EI \), is \( 16.66 \times 10^5 \, {Nm}^2 \) and the length of the beam \( L \) is 1 m.
The deflection at the loading point is ............ mm (rounded off to two decimal places).
In the figures given below, L and H indicate low and high pressure centers, respectively; PGF, CoF and CeF indicate Pressure Gradient Force, Coriolis Force and Centrifugal Force, respectively; \( V \) is Velocity. [The arrows indicate only the directions but not the magnitudes of the forces and velocity.]
Which of the following is/are the correct representation(s) of the directions of various forces and velocity in the gradient wind balance in the northern hemisphere?
Which of the following is the correct form of the mass divergence form of the continuity equation for a compressible fluid? [In the given equations, \( \rho \) is the density and \( \nabla \) the three-dimensional velocity vector of the fluid.]
[(i)] $\displaystyle \frac{\partial \rho}{\partial t} + \nabla \times (\rho \mathbf{v}) = 0$
[(ii)] $\displaystyle \frac{\partial \rho}{\partial t} + \nabla \cdot (\rho \mathbf{v}) = 0$
[(iii)] $\displaystyle \frac{\partial \mathbf{v}}{\partial t} + \rho \cdot \nabla \mathbf{v} = 0$
[(iv)] $\displaystyle \frac{\partial \rho}{\partial t} + \mathbf{v} \cdot \nabla \rho = 0$
The vertical (depth) profiles for three parameters P1, P2, and P3 in the northern Indian Ocean are given in the figure below. The values along the x-axis are the normalized values of the parameters and y-axis is the depth (m).
Identify the parameters P1, P2, and P3 from the options given below.