Group-I shows different two-dimensional bodies and Group-II mentions their total drag coefficient \( C_d \) based on frontal area while facing parallel flow of fluid having Reynolds number \( Re \geq 10^4 \) along the direction of the arrow. The bodies are placed symmetrically with respect to the flow direction. Which one of the following options identifies the correct match between Group-I and Group-II, as per the concept of degree of streamlining?
In fluid dynamics, the drag coefficient \( C_d \) is a measure of the resistance experienced by an object as it moves through a fluid. The degree of streamlining of an object is directly related to its drag coefficient—streamlined objects tend to have lower drag coefficients.
Let’s analyze each case step by step:
1. \( P \) - Square Cylinder (Flow direction: right):
The square cylinder has the highest drag coefficient among all the shapes, because the sharp corners and flat surfaces create significant resistance to the flow of fluid. Therefore, the drag coefficient for \( P \) is the highest, which is \( 2.1 \), and this shape is the least streamlined.
2. \( Q \) - Square Cylinder (Flow direction: top-right):
When the square cylinder faces the flow at an angle (like in \( Q \)), it still experiences a significant drag, but slightly less than the one facing directly. Hence, the drag coefficient for \( Q \) is \( 1.6 \).
3. \( R \) - Half Tube (Flow direction: left):
The half-tube shape is more streamlined than the square cylinders. The fluid flow around the half-tube is more continuous and experiences less resistance, making the drag coefficient lower. For \( R \), the drag coefficient is \( 1.2 \), which is the lowest among the shapes listed.
4. \( S \) - Half Tube (Flow direction: right):
The half-tube facing the flow from the right (as in \( S \)) has a drag coefficient of \( 2.3 \), which is still lower than the square cylinders but higher than the half-tube facing the flow from the left. Based on this analysis, the correct matching is: \[ P = 3 ({Square Cylinder with the highest drag coefficient}) \] \[ Q = 2 ({Square Cylinder with a slightly lower drag coefficient}) \] \[ R = 1 ({Half Tube with the lowest drag coefficient}) \] \[ S = 4 ({Half Tube facing the flow from the right}) \] Thus, the correct match between Group-I and Group-II is: \( P = 3, Q = 2, R = 1, S = 4 \).
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)
Figure shows the steady and incompressible flow of a fluid in the direction of the arrow from section A to section D. Three pipe connectors are to be placed between sections at A and D having Total Energy Line (TEL) and Hydraulic Grade Line (HGL) as depicted in the figure. Consider, \( g \), \( P \), \( Q \), \( V \), \( \gamma \), and \( Z \) denote gravitational acceleration, pressure, volume flow rate, velocity, specific weight, and elevation of the centerline of the pipe connectors from the datum, respectively. Which one of the following options, in sequence, indicates the correct nature of connectors between sections A and B, B and C, and C and D in the direction of flow?
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.