Important Derivations: Mechanical Properties of Fluids | Physics Class 11 - NEET PDF Download

Derivation of Stoke’s Law

What is Stoke’s Law?

Stoke’s Law is a mathematical equation that expresses the settling velocities of the small spherical particles in a fluid medium. The law is derived considering the forces acting on a particular particle as it sinks through the liquid column under the influence of gravity. The force that retards a sphere moving through a viscous fluid is directly proportional to the velocity and the radius of the sphere, and the fluid’s viscosity.

Stoke’s Law Equation

Sir George G. Stokes, an English scientist, clearly expressed the viscous drag force F as:

Where r is the sphere radius, η is the fluid viscosity, and v is the sphere’s velocity.

Stoke’s Law Derivation

From Stoke’s Law viscosity equation, we know that viscous force acting on a sphere is directly proportional to the following parameters:

• the radius of the sphere (r)
• coefficient of viscosity (η)
• the velocity of the object (v)

Mathematically, this is represented as

Now let us evaluate the values of a, b and c.
Substituting the proportionality sign with an equality sign, we get

Here, k is the constant of proportionality, a numerical value with no dimensions.
Writing the dimensions of parameters on either side of equation (1), we get
[MLT^–2] = [ML^–1T^–1]^a [L]^b [LT^-1]^c
Simplifying the above equation, we get
[MLT^–2] = M^a ⋅ L^–a+b+c ⋅ T^–a–c… (2)
According to classical mechanics, mass, length and time are independent entities.
Equating the superscripts of mass, length and time, respectively from equation (2), we get
a = 1… (3)
–a + b + c = 1… (4)
–a –c = -2 or a + c = 2… (5)
Substituting (3) in (5), we get
1 + c = 2
c = 1 (6)
Substituting the value of (3) & (6) in (4), we get
–1 + b + 1 = 1
b = 1 (7)
Substituting the value of (3), (6) and (7) in (1), we get

The value of k for a spherical body was experimentally obtained as
6π
Therefore, the equation gives the viscous force on a spherical body falling through a liquid.

What is Reynolds Number?

Reynolds number referred to as Re is a dimensionless quantity which is used in fluid mechanics to predict the flow patterns in different fluid flow conditions. It is defined as the ratio of inertial force to viscous force within the fluid. The mathematical representation is given as:

Where,

• ⍴ is the density of the fluid in kg.m^-3
• 𝜇 is the dynamic viscosity of the fluid in N.s.m^-2
• 𝜈 is the kinematic viscosity of the fluid in m².s^-1
• u is the velocity of a fluid with respect to the object in m.s^-1
• L is the characteristic linear dimension in m

Using Reynolds number, it becomes easy to determine whether the fluid flow is laminar or turbulent. Following are the boundary values of a circular pipe that can be used to determine the flow pattern:

• If Re > 2300, then the flow is said to be laminar.
• If 2300 < Re < 4000, then the flow is said to be transient.
• If Re > 4000, then the flow is said to be turbulent.

Reynolds Number Derivation

The mathematical form of the Reynolds number can be derived as follows:
R_e = inertial force/viscous force




Where,

• t is the time
• y is the cross-sectional position
• 
  is the flow speed
• τ is the shear stress in Pa
• A is the cross-sectional area of the flow
• V is the volume of the fluid element
• L is the characteristic linear dimension in m
• u₀ is the maximum speed of the object relative to the fluid in m.s^-1
• ⍴ is the density of the fluid in kg.m^-3
• 𝜇 is the dynamic viscosity of the fluid in N.s.m^-2
• 𝜈 is the kinematic viscosity of the fluid in m².s^-1

Following is the Reynolds number representation for the flow in a pipe:



Where,

• D_H is the hydraulic diameter of the pipe in m
• Q is the volumetric flow rate in m³.s^-1
• A is the pipe’s cross-sectional area in m²
• u is the mean velocity of the fluid in m.s^-1
• ⍴ is the density of the fluid in kg.m^-3
• 𝜇 is the dynamic viscosity of the fluid in N.s.m^-2
• 𝜈 is the kinematic viscosity of the fluid in m².s^-1

Critical Reynolds number and hydraulic diameter

Critical Reynold number of any fluid flow is defined when the flow pattern changes from laminar to turbulent. It is referred to as Re_cr. The critical Reynold number is not fixed as it varies from geometry to geometry and also is dependent on flow conditions.
For a circular pipe, the critical Reynolds number is given as Re_cr=2300 and for non-circular pipes it depends on the hydraulic diameter D_h which is defined as

Where,
A_c is the cross-sectional area of the pipe
P is the wetted perimeter of the pipe
Hydraulic radius is defined as the cross-sectional area of the channel divided by the wetted perimeter and referred as R_H.

Following is the table of hydraulic diameter of non-circular tubes and channels:

Reynolds Number Examples

Example 1: A Newtonian fluid with a dynamic viscosity of 0.40 n.s.m^-2 and a specific gravity of 0.93 flows through a 28 mm diameter pipe with a velocity of 2.9 m.s^-1.
Ans: The density can be calculated using the specific gravity like
⍴=0.93(1000kg.m^-3)
=930kg.m^-3
The Reynolds number can be calculated using the formula as

R_e=(930kg.m^-3) (2.9m.s^-1) (28mm) (10^-3m.mm^-1)/(0.38Ns.m^-2)
= 198 (kg.m.s^-2)/N
Since R_e=198 the flow is laminar.

Example 2: A person turns on the water tap in his kitchen. Water flows out from a copper pipe with 7.00 mm diameter at a velocity of 1.00 ms^-1. The density of water in the pipe is 1000kg.m^-3 and viscosity 0.00135 Pa.s^-1. What is the Reynolds number, and what is the type of flow in the pipe?
Ans: The diameter of the pipe=7.00 mm = 0.007 m
Using Reynolds number formula:

R_e=(1000kg.m^-3) (1.00m.s^-1) (0.007m)/0.00135 Pa.s^-1
=(1000kg.m^-3) (1.00m.s^-1) (0.007m)/0.00135 kg.m^-1.s^-1
=5185
Since R_e=5185 the flow is turbulent.

Terminal Velocity Derivation

What is Terminal Velocity?

Terminal velocity is defined as the highest velocity attained by an object falling through a fluid. It is observed when the sum of drag force and buoyancy is equal to the downward gravity force acting on the object. The acceleration of the object is zero as the net force acting on the object is zero.

How to find Terminal Velocity?

In fluid mechanics, for an object to attain its terminal velocity, it should have a constant speed against the force exerted by the fluid through which it is moving.
The mathematical representation of terminal velocity is:

Where,
vt is the terminal velocity, m is the mass of the falling object, g is the acceleration due to gravity, Cd is the drag coefficient, 𝜌 density of the fluid through which the object is falling, and A is the area projected by the object.

Terminal Velocity Derivation

Deriving terminal velocity using mathematical terms according to the drag equation as follows:
F = bv2
Where b is the constant depending on the type of drag

(integrating the equations)

Where,

After integration,

After substituting for v_t

Therefore, above is the derivation of terminal velocity.

Derivation of Continuity Equation

According to the continuity equation, the product of the cross-sectional area of the pipe and the velocity of the fluid at any given point along the pipe is constant.

Continuity Equation Derivation

Continuity equation represents that the product of cross-sectional area of the pipe and the fluid speed at any point along the pipe is always constant. This product is equal to the volume flow per second or simply the flow rate.  The continuity equation is given as:
R = A v = constant
Where,

• R is the volume flow rate
• A is the flow area
• v is the flow velocity

Assumption of Continuity Equation

Following are the assumptions of continuity equation:

• The tube is having a single entry and single exit
• The fluid flowing in the tube is non-viscous
• The flow is incompressible
• The fluid flow is steady

Derivation

Consider the following diagram:
Equation of Continuity

Now, consider the fluid flows for a short interval of time in the tube. So, assume that short interval of time as Δt. In this time, the fluid will cover a distance of Δx₁ with a velocity v₁ at the lower end of the pipe.
At this time, the distance covered by the fluid will be:
Δx₁ = v₁Δt
Now, at the lower end of the pipe, the volume of the fluid that will flow into the pipe will be:
V = A₁ Δx₁ = A₁ v₁ Δt
It is known that mass (m) = Density (ρ) × Volume (V). So, the mass of the fluid in Δx₁ region will be:
Δm₁= Density × Volume
⇒ Δm₁ = ρ₁A₁v₁Δt ——–(Equation 1)
Now, the mass flux has to be calculated at the lower end. Mass flux is simply defined as the mass of the fluid per unit time passing through any cross-sectional area. For the lower end with cross-sectional area A₁, mass flux will be:
Δm_{1/Δt =} ρ₁A₁v₁ ——–(Equation 2)
Similarly, the mass flux at the upper end will be:
Δm_2/Δt = ρ₂A₂v₂ ——–(Equation 3)
Here, v₂ is the velocity of the fluid through the upper end of the pipe i.e. through Δx₂ , in Δt time and A₂, is the cross-sectional area of the upper end.
In this, the density of the fluid between the lower end of the pipe and the upper end of the pipe remains the same with time as the flow is steady. So, the mass flux at the lower end of the pipe is equal to the mass flux at the upper end of the pipe i.e. Equation 2 = Equation 3.
Thus,
ρ₁A₁v_{1 =} ρ₂A₂v₂ ——–(Equation 4)
This can be written in a more general form as:
ρ A v = constant
The equation proves the law of conservation of mass in fluid dynamics. Also, if the fluid is incompressible, the density will remain constant for steady flow. So, ρ₁ =ρ₂.
Thus, Equation 4 can be now written as:
A₁ v_{1 =} A₂ v₂
This equation can be written in general form as:
A v = constant
Now, if R is the volume flow rate, the above equation can be expressed as:
R = A v = constant
This was the derivation of continuity equation.

Continuity Equation in Cylindrical Coordinates

Following is the continuity equation in cylindrical coordinates:

Incompressible Flow Continuity Equation

Following is the continuity equation for incompressible flow as the density, ρ = constant and is independent of space and time, we get:
∇.v = 0

Steady Flow Continuity Equation

Following is the continuity equation in cylindrical coordinates: