Step 1: Understand terminal velocity and Stokes’ law.
The terminal velocity of a small sphere settling in a viscous fluid occurs when the gravitational force (minus buoyancy) is balanced by the drag force, so the sphere falls at a constant velocity. For small spheres under laminar flow conditions (low Reynolds number, \( \text{Re}<1 \)), Stokes’ law applies. The terminal velocity (\( v_t \)) is given by: \[ v_t = \frac{g (\rho_s - \rho_f) d^2}{18 \mu}, \] where:
\( g \): gravitational acceleration (\( \text{m/s}^2 \)),
\( \rho_s \): density of the sphere (\( \text{kg/m}^3 \)),
\( \rho_f \): density of the fluid (\( \text{kg/m}^3 \)),
\( d \): diameter of the sphere (\( \text{m} \)),
\( \mu \): viscosity of the fluid (\( \text{Pa·s} \)).
Step 2: Analyze the dependency of terminal velocity.
From Stokes’ law, \( v_t = \frac{g (\rho_s - \rho_f) d^2}{18 \mu} \), we can determine how \( v_t \) varies with each parameter:
Diameter (\( d \)): \( v_t \propto d^2 \), so terminal velocity varies as the square of the diameter, not the first power.
Viscosity (\( \mu \)): \( v_t \propto \frac{1}{\mu} \), so terminal velocity varies as the inverse of the fluid viscosity.
Difference in densities (\( \rho_s - \rho_f \)): \( v_t \propto (\rho_s - \rho_f) \), which is related to the difference in specific weights (since specific weight is \( \rho g \)), but it is a linear relationship, not squared.
Step 3: Evaluate the options.
(1) First power of its diameter: Incorrect, as \( v_t \propto d^2 \), not \( d \). Incorrect.
(2) Inverse square of its diameter: Incorrect, as \( v_t \propto d^2 \), not \( \frac{1}{d^2} \). Incorrect.
(3) Inverse of the fluid viscosity: Correct, as \( v_t \propto \frac{1}{\mu} \), matching the inverse relationship with viscosity. Correct.
(4) Square of the difference in specific weight of solid and fluid: Incorrect, as \( v_t \propto (\rho_s - \rho_f) \), a linear relationship, not squared. Incorrect.
Step 4: Select the correct answer.
The terminal velocity of a small sphere settling in a viscous fluid varies as the inverse of the fluid viscosity, matching option (3).
A fixed control volume has four one-dimensional boundary sections (1, 2, 3, and 4). For a steady flow inside the control volume, the flow properties at each section are tabulated below:
The rate of change of energy of the system which occupies the control volume at this instant is \( E \times 10^6 \, {J/s} \). The value of \( E \) (rounded off to 2 decimal places) is ........
A liquid flows under steady and incompressible flow conditions from station 1 to station 4 through pipe sections P, Q, R, and S as shown in the figure. Consider, \( d \), \( V \), and \( h \) represent the diameter, velocity, and head loss, respectively, in each pipe section with subscripts ‘P’, ‘Q’, ‘R’, and ‘S’. \( \Delta h \) represents the head difference between the inlet (station 1) and outlet (station 4). All the pipe sections are placed on the same horizontal plane for which the figure shows the top view.
(Insert diagram here, if possible)
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