Step 1: Given data:
Density \( \rho = 870 \, {kg/m}^3 \),
Viscosity \( \mu = 0.036 \, {Pa.s} \),
Diameter \( D = 0.1 \, {m} \),
Length \( L = 1.5 \, {km} = 1500 \, {m} \),
Flow rate \( Q = 250 \, {L/min} = \frac{250}{1000 \times 60} = \frac{1}{240} \, {m}^3/{s} \),
Total head loss = 11.60 m,
Acceleration due to gravity \( g = 10 \, {m/s}^2 \)
Step 2: Velocity in the pipe:
\[ A = \frac{\pi D^2}{4} = \frac{\pi (0.1)^2}{4} = \frac{\pi}{400} \, {m}^2 V = \frac{Q}{A} = \frac{1/240}{\pi/400} = \frac{400}{240\pi} \approx 0.53 \, {m/s} \]
Step 3: Calculate Reynolds number:
\[ Re = \frac{\rho V D}{\mu} = \frac{870 \cdot 0.53 \cdot 0.1}{0.036} \approx 1279.17 \]
Since \( Re<2000 \), the flow is laminar.
Step 4: Head loss due to pipe (major loss):
For laminar flow, Darcy's friction factor \( f = \frac{64}{Re} \approx \frac{64}{1279.17} \approx 0.050 \)
Using Darcy–Weisbach equation: \[ h_f = f \cdot \frac{L}{D} \cdot \frac{V^2}{2g} h_f = 0.050 \cdot \frac{1500}{0.1} \cdot \frac{(0.53)^2}{2 \cdot 10} \approx 10.7 \, {m} \]
Step 5: Minor head loss due to valve: \[ h_{{minor}} = h_{{total}} - h_{{major}} = 11.60 - 10.7 = 0.90 \, {m} \]
Suppose that 2 is an eigenvalue of the matrix
Then the value of \( \alpha \) is equal to (Answer in integer):
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)] $\displaystyle \frac{\partial \rho}{\partial t} + \mathbf{v} \cdot \nabla \rho = 0$