Short Notes: Fluid Kinematics | Fluid Mechanics for Mechanical Engineering PDF Download

Introduction

Fluid Kinematics deals with the motion of fluids such as displacement, velocity, acceleration, and other aspects. This topic is useful in terms of exams and knowledge of the candidate.

Kinematics is the branch of classical mechanics that describes the motion of bodies and systems without consideration of the forces the cause the motion.

Types of Fluid Flows

Fluid flow may be classified under the following headings:

1. Steady & Unsteady Flow

2. Uniform and Non-Uniform Flow

3. Laminar and Turbulent Flow

4. Rotational & Irrotational Flow

Combining these, the most common flow types are:

(a) Steady uniform flow

• Conditions do not change with position in the stream or with time.
  Example: flow of water in a pipe of constant diameter at a constant velocity.

Steady Uniform Flow

(b) Steady non-uniform flow

• Conditions change from point to point in the stream but do not change with time.
  Example: Flow in a tapering pipe with constant velocity at the inlet.

(c) Unsteady uniform flow

• At a given instant in time the conditions at every point are the same but will change with time.
  Example: A pipe of constant diameter connected to a pump pumping at a constant rate which is then switched off.

(d) Unsteady non-uniform flow

• Every condition of the flow may change from point to point and with time at every point.
  Example: Waves in a channel

Flow Pattern

• Pathline is the actual path traveled by an individual fluid particle over some time period. The pathline of a fluid element A is simply the path it takes through space as a function of time. An example of a pathline is the trajectory taken by one puff of smoke which is carried by the steady or unsteady wind.
• Timeline is a set of fluid particles that form a line at a given instant.
• Streamline is a line that is everywhere tangent to the velocity field. Streamlines are obtained analytically by integrating the equations defining lines tangent to the velocity field as illustrated in the figure below:
  where u, v, and w are the velocity components in x, y and z directions respectively as sketched.
• Streakline is the locus of particles that have earlier passed through a prescribed point.
  a. A streakline is associated with a particular point P in space which has the fluid moving past it.
  b. All points which pass through this point are said to form the streakline of point P.
  c. An example of a streakline is the continuous line of smoke emitted by a chimney at point P, which will have some curved shape if the wind has a time-varying direction.
• Streamtube: The streamlines passing through all these points form the surface of a stream-tube. Because there is no flow across the surface, each cross-section of the stream tube carries the same mass flow. So the stream tube is equivalent to a channel flow embedded in the rest of the flow field.
  

Note: The figure below illustrates streamlines, pathlines, and streaklines for the case of a smoke being continuously emitted by a chimney at point P, in the presence of a shifting wind.

In a steady flow, streamlines, pathlines, and streaklines all coincide.

In this example, they would all be marked by the smoke line.

Velocity of Fluid Particle

• Velocity of a fluid along any direction can be defined as the rate of change of displacement of the fluid along that direction.
• Let V be the resultant velocity of a fluid along any direction and u, v and w be the velocity components in x, y and z directions respectively.
• Mathematically the velocity components can be written as:
  u = f ( x, y, z, t )
  w = f ( x, y, z, t )
  v = f ( x, y, z, t )
• Let VR is resultant velocity at any point in a fluid flow. 
• Resultant velocity V_R = ui + vj + wk
  

Where u = dx/dt, v = dy/dt and w = dz/dt are the resultant vectors in X, Y and Z directions, respectively.

Acceleration of Fluid Particle

• Acceleration of a fluid element along any direction can be defined as the rate of change of velocity of the fluid along that direction.
• If a_x , a_y and a_z are the components of acceleration along x, y and z directions respectively, they can be mathematically written as a_x  = du/ dt.
  

Stream Function

• The partial derivative of stream function with respect to any direction gives the velocity component at right angles to that direction. It is denoted by ψ.
  
• Continuity equation for two-dimensional flow is:
  

Equations of Rotational Flow

• As ψ satisfies the continuity equation hence if ψ exists then it is a possible case of fluid flow.
• Rotational components of fluid particles are:
  
  
  

Equation of Irrotational Flow

• If ω_x = ω_y = ω_z then, flow is irrotational.
• For irrotational flow, ωz = 0
  
  
  
• This is Laplace equation for ψ.

Note: It can be concluded that if stream function (ψ) exits, it is a possible case of fluid flow. But we can’t decide whether flow is rotational or irrotational. But if stream function ψ satisfies Laplace equation then, it is a possible case of irrotational flow otherwise it is rotational flow.

Velocity Potential Function

It is a scalar function of space and time such that its negative derivative with respect to any direction gives the fluid velocity in that direction. It is denoted by φ.

We know that continuity equation for steady flow is:

• If φ satisfies the Laplace equation, then it is a possible case of fluid flow.

Rotational component ω_z can be given by:

It shows that φ exits then, flow will be irrotational.

Relation between Stream Function and Velocity Potential

We know,

and

Stream versus Velocity Function

Example 1: The velocity field of a two-dimensional, incompressible flow is given by

where denote the unit vectors in x and y directions, respectively. If v(x,0)=coshx, then v ( 0 , − 1 ) v(0,−1)
(a) 1
(b) 2
(c) 3
(d) 4
Ans: (c)
Solution:
For an incompressible flow,
Given; the velocity field of a two-dimensional, incompressible flow,

Now, (for an incompressible flow)

Integrate both sides,

Now, from equation (1)


Example 2: Consider a unidirectional fluid flow with the velocity field given by

where  u(0,t)=1. If the spatially homogeneous density field varies with time  t as

the value of u(2,1) is _______. (Rounded off to two decimal places)
Assume all quantities to be dimensionless.
(a) 1.14
(b) 2.25
(c) 3.65
(d) 8.25
Ans: (a)
Continuity equation for unsteady flow


Since


Example 3: The velocity field of a certain two-dimensional flow is given by

where k=2s ⁻¹ . The coordinates  x and y are in meters. Assume gravitational effects to be negligible. If the density of the fluid is 1000kg/m ³ and the pressure at the origin is 100 kPa, the pressure at the location (2 m, 2 m) is _____________ kPa. (Answer in integer)
(a) 64
(b) 26
(c) 84
(d) 98
Ans: (c)
Solution:
To find the pressure at location (2m,2m) we apply Bernouli's equation

We will apply this equation between two points Origin (0,0) and location (2 m,2 m)
At Origin (0,0)

At Iocation (2,2)

magnitude of velocity

Applying Bernouli's theorem