# Control Volume Analysis

By Mukul Yadav|Updated : December 20th, 2022

Control volume analysis is the analysis of the control volume considered in the analysis of the pipe flow. A control volume is a volume in space considered for analyzing a particular term. In fluid mechanics, the control volume is considered to analyze the different losses in the pipe flow. The control volume analysis is required before the analysis of the pipe flow.

### Control Volume Analysis PDF

Control volume analysis is the process of analyzing a control volume, which is established with the help of mathematical tools. With respect to the internal frame of reference, the control volume is assumed to be fixed, or it can be considered to be moving at the same speed as the fluid. This article contains basic notes on the "Control Volume Analysis" topic of the "Fluid Mechanics & Hydraulics" subject.

## What is Control Volume Analysis?

Control Volume Analysis of Mass, Momentum, and Energy is an important topic of Fluid mechanics that deals with control mass, control volume, momentum equation, continuity equation, and Impact of Jets on planes and vanes. Control volume analysis is the analysis of the control volume, and it is carried out with the help of various mathematical tools. It is required to establish the control volume.

### Control Mass

• A fixed mass of a fluid element in the flow field is identified, and conservation equations for properties such as momentum, energy, or concentration are written.
• The identified mass moves around in the flow field.
• Its property corresponds to the same contents of the identified fluid element that may change from one location to another.

### Control Volume

• This approach is popular and widely applied in the analysis.
• An arbitrarily fixed volume located at a certain place in the flow field is identified, and the conservation equations are written.
• The property under consideration or analysis may change with time.

## Momentum Equation in Control Volume Analysis

It is based on the law of conservation of momentum or on the momentum principle, which states that the net force acting on a fluid mass is equal to the change in momentum of flow per unit of time in that direction.

F.dt = d(mv) ………… (1)

which is known as the impulse-momentum equation and states that the impulse of a force F acting on a fluid of mass m in a short interval of time dt is equal to the change of momentum d(mv) in the direction of the force.

### Force exerted by a flowing fluid on a pipe bend.

The impulse-momentum equation (1) determines the resultant force exerted by a flowing fluid on a pipe bend. Let v1, p1 and A1 are the velocity, pressure and area at section 1 of the pipe.

and v2, p2, A2 = corresponding values of velocity, pressure and area in section (2).

Let Fx = horizontal component of the force exerted by the fluid element on the bend in the x-direction.

Fy = vertical component of the force exerted by fluid element on the bend in the y-direction

The momentum equation in the x-direction is given by,

P1A1 - P2A2 cosθ - Fx = ρQ (V2Cosθ- V1) ……………… (2)

Similarly, the momentum equation in the y-direction gives

P2A2 sinθ - Fy = ρQ (V2 sinθ - 0) ………………. (3)

Fy = ρQ (- V2 sinθ) - P2A2sinθ

Now the resultant force (FR) acting on the bend,

FR= (F2x + F2y)0.5

And the angle made by the resultant force with horizontal direction is given by

tanθ = Fy/Fx

### Moment of Momentum Equation

The moment of momentum equation is derived from the moment of momentum principle, which states that the resulting torque acting on a rotating fluid equals the rate of change of the moment of momentum.

According to the moment of momentum principle,

Resultant torque = rate of change of moment of momentum

T = ρQ [V2r2 - V1r1]

The momentum equation relates the sum of the forces to the acceleration or rate of change of momentum From the conservation of mass,

mass into face 1 = mass out of face 2

The rate at which momentum enters face 1 is

ρ1A1u1u1 = mu1

The rate at which momentum leaves face 2 is

ρ2A2u2u2 = mu2

Thus the rate at which momentum changes across the stream tube is

ρ2A2u2u2 - ρ1A1u1u1 = mu2 - mu1

The Momentum equation is:

F = m(u2 - u1)

F = Qρ(u2 - u1)

This force acts on the fluid in the direction of the flow of the fluid

• If the Motion is not one-dimensional. We consider the forces by resolving in the directions of the coordinate axes.

The force in the x-direction

Fx = m(u2 cosθ2 - u1 cosθ1)

= m(u2x - u1x)

or

Fx = Qρ(u2 cosθ2 - u1 cosθ1)

= Qρ(u2x - u1x)

And the force in the y-direction

Fy = m=u2 sinθ2 - u1 sinθ1)

= m(u2y - u1y)

or

Fy = Qρ(u2 sinθ2 - u1 sinθ1)

= Qρ(u2y - u1y)

The resultant force can be found by combining these components. ## Application of Momentum Equation

The momentum equation has various applications in fluid mechanics problems. With the help of the momentum equation, a very complex problem can be solved easily. Here momentum equations are explained for the condition of a pipe flow in different conditions.

### Force due to the flow around a pipe bend

A converging pipe bend lying in the horizontal plane turning through an angle of Θ. • As the fluid changes direction, a force will act on the bend.
• This force can be very large in the case of water supply pipes. The bend must be held in place to prevent breakage at the joints.

### Taking Control Volume

In the x-direction

FTx = ρQ(u2x - u1x)

u1x = u1

u2x = u2 cosθ

FTx = ρQ(u2 cosθ - u1)

In the y-direction

FTy = ρQ(u2y - u1y)

u1y = u1sin 0 = 0

u2y = u2 sinθ

FTy = ρQ(u2 sinθ - u1)

It can also be written by using Bernoulli Equations where hf is the friction loss (this can often be ignored, hf=0)

As the pipe is in the horizontal plane, z1=z2 And with continuity, Q= u1A1 = u2A2 Knowing the pressures at each end, the pressure force can be calculated,

FP = Pressure force at 1 - Pressure force at 2

FPx = ρ1A1 cos 0 - ρ2A2 cosθ = ρ1A1 - ρ2A2 cosθ

FPy = ρ1A1 sin 0 - ρ2A2 sinθ = - ρ2A2 sinθ

There are no body forces in the x or y directions, so FRx = FRy = 0

The body force due to gravity is acting in the z-direction, so it need not be considered

FRx = FTx - FPx - 0

= ρQ(u2 cosθ - u1) - ρ1A1 + ρ2A2 cosθ

FRy = FTy - FPy - 0

= ρQu2 sinθ + ρ2A2 sinθ

The resultant force on the fluid is given by ## Impact of a Jet on a Plane

To determine the impact force of a jet on a plane, we also require the control volume analysis of the flow. The impact force on a jet can be calculated by equating the total energy of the flow before and after the striking of the flow with the help. It is explained below with detailed information.

### A jet hitting a flat plate (a plane) at an angle of 90º

The reaction force of the plate. i.e., the force the plate will have to apply to stay in the same position In the x-direction

FTx = ρQ(u2x - u1x)

FTx = -ρQu1x

The system is symmetrical, so the forces in the y-direction cancel, so Fy = 0

The pressures at the inlet and the outlets to the control volume are atmospheric. So, the pressure force is zero.

Fpx= Fpy= 0

As the control volume is small, we can ignore the body force due to gravity, FBx= FBy= 0

FTx = FRx + FPx + FBx

FRx = FTx - 0 - 0

FRx = -ρQu1x

## Force on a Curved Vane

Force on a curved vane can be calculated with the control volume analysis of the flow. With the help of momentum equations in both directions, it can be calculated easily. The force calculation on a curved vane is explained below in detail.

• Pressures at ends are equal, which is equal to atmospheric pressure.
• The cross-section and velocities (in the flow direction) remain constant. Total force in the x-direction

FTx = ρQ(u2 - cosθ)

by continuity equation, u1 = u2 = Q/A

FTx = -ρQ2(1 - cosθ)/A

In the y-direction

FTy = ρQ(u2 sinθ- 0)

FTy = ρQ2/A

• The pressure at the inlet and the outlets to the control volume are atmospheric, Fpx=Fpy=0.
• Nobody forces in the x-direction, FBx=0
• In the y-direction, the body force acting is the weight of the fluid.
• If V is the volume of the fluid on the vane, then FBX= ρgV.

The resultant force in all directions are

FTx = FRx + FPx +FBx

FRx = FTx = -ρQ2(1 - cosθ)/A

FTy = FRy + FPy +FBy

FTy = FRy = ρQ2/A

And the resultant force on the fluid is given by The force on the vane is the same magnitude but in the opposite direction, R= -FR.

### Force Exerted by the Jet on a Stationary Vertical Plate

Consider a jet of Water coming out from the nozzle strikes a flat vertical plate, Fx = ρaV[V – 0]

Fx = ρaV2

Force exerted by the jet on a curved plate(vane) when the plate/vane is moving in the direction of the jet,  ### Force Exerted by a Jet on a Hinged Plate

Consider a jet of water striking a vertical plate at the center which is hinged at O. Due to the force exerted by the jet on the plate, the plate will swing through some angle about the hinge, as shown in Fig.  Other Important GATE Notes Steel Zero Force Member In A Truss Functions Of The Network Layer Transverse Loading Geometric Design Of Highways Moment Area Method Macaulay's Method Impact Load Impulse An Momentum Uniformly Varying Load

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## FAQs on Control Volume Analysis

• Control volume analysis is the analysis of the control volume. It can be used for the analysis of a particular topic. It is determined with the help of mathematical tools and expressions.

• Control volume analysis of momentum is used to analyze the different losses in pipe flow. The momentum equation for the fluid flow can be written based on the total energy of the flow.

• Control valume analysis is carried out based on the control volume. And control volume is determined based on the suitability of the cross section which is considered for the analysis.

• Generally, two types of control volume are considered for the analysis of different parameters in the analysis of a problem in fluid dynamics. These types of control volume are communally known as Lagrangian and Eulerian types.

• The analysis of different parameters like losses that occurred in flow etc. can be easily analyzed with the help of control volume analysis. In control volume flow mass is entered from one side and out from other side.

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