elementary fluid mechanics by rasikh tariq

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Page 1: Elementary Fluid Mechanics by Rasikh Tariq

E l e m e n t a r y F l u i d M e c h a n i c s

By Rasikh Tariq

1Department of Mechanical Engineering - Mohammad Ali Jinnah University, Islamabad Campus

Page 2: Elementary Fluid Mechanics by Rasikh Tariq

Concept of Streamline & Normal

The lines that are tangent to the velocity Vectors throughout the flow field.

2

Page 3: Elementary Fluid Mechanics by Rasikh Tariq

Balancing Newton’s 2nd Law

Assumptions

3

Inviscid Fluid Analysis Steady-Flow Analysis

Inviscid Fluid Analysis:- The Fluid is assumed to have ZERO Viscosity.

Steady Flow Analysis:-Fluid properties (Either Intensive or Extensive) that are

independent of TIME.

Page 4: Elementary Fluid Mechanics by Rasikh Tariq

Balancing Newton’s 2nd Law

4

Page 5: Elementary Fluid Mechanics by Rasikh Tariq

Balancing Newton’s Law Normal to Streamline

5

Page 6: Elementary Fluid Mechanics by Rasikh Tariq

Balancing Newton’s Law Normal to Streamline

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The equation tells us Pressure Variation along the path Normal to Streamline. i.e Depending On the Path.

Assumptions:- Inviscid Flow Steady-flow Fluid Analysis Valid for Fluids that are only experiencing Pressure & Weight.

Page 7: Elementary Fluid Mechanics by Rasikh Tariq

Balancing Newton’s 2nd Law Along the Streamline

7

Pressure Variation Along the Streamline i.e. Path Function

Across 2 different Points i.e. Point Function

Assumptions:- Invscid Flow Analysis Steady Flow Analysis

is also Bernoulli's Equation.

Page 8: Elementary Fluid Mechanics by Rasikh Tariq

Further Assumption – Bernoulli's Equation

8

For Incompressible Flow i.e. Density is constant along the Streamline

is also Bernoulli's Equation.

Assumptions:- Inviscid Flow Analysis Steady Flow Analysis Incompressible Fluid Analysis Only applicable along the Streamline

Restrictions:- Rotational Effects Concept of Vorticity No External Mechanical Devices

(Pumps & Turbines)

Page 9: Elementary Fluid Mechanics by Rasikh Tariq

Effects of Compressibility

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For Incompressible Flow i.e. Density is constant along the Streamline

Assumptions:- Compressible Isentropic (Internally Reversible & Adiabatic Process or constant

Entropy) Steady Flow

k=Where

Page 10: Elementary Fluid Mechanics by Rasikh Tariq
Page 11: Elementary Fluid Mechanics by Rasikh Tariq

Concept of Stagnation Point

11

Fluid Velocity is ZERO at Stagnation Point.

Page 12: Elementary Fluid Mechanics by Rasikh Tariq

Applying Bernoulli's Equation

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Stagnation Point

Page 13: Elementary Fluid Mechanics by Rasikh Tariq

Applying Bernoulli's Equation- Free Jet

13

d

1

2

h

By Balancing Bernoulli's Equation, we get.

Page 14: Elementary Fluid Mechanics by Rasikh Tariq

Applying Bernoulli's Equation- Free Jet

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Co-efficient of Contraction

Page 15: Elementary Fluid Mechanics by Rasikh Tariq

Applying Bernoulli's Equation- Free Jet

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Co-efficient of Contraction

Page 16: Elementary Fluid Mechanics by Rasikh Tariq

Applying Bernoulli's Equation- Free Jet

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Co-efficient of Contraction

Page 17: Elementary Fluid Mechanics by Rasikh Tariq

Applying Bernoulli's Equation- Free Jet

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Co-efficient of Contraction

Page 18: Elementary Fluid Mechanics by Rasikh Tariq

Flow Rate Measurement – Closed Channel

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Balancing Bernoulli's Eq

0 0

Further Simplifying using

We come up with

Page 19: Elementary Fluid Mechanics by Rasikh Tariq

Flow Rate Measurement – Closed Channel

19

Open Channel (Lower Stream)

Sluice Gate

And

We come up to the Result

Note : But make sure, Never forget all the Assumptions

Page 20: Elementary Fluid Mechanics by Rasikh Tariq

Flow Rate Measurement – Closed Channel

20

Open Channel (Upper Stream)

Weir

Page 21: Elementary Fluid Mechanics by Rasikh Tariq

Flow Rate Measurement – Closed Channel

21

Open Channel (Upper Stream)

Weir

And

We come up to the Result

Note : But make sure, Never forget all the Assumptions

Page 22: Elementary Fluid Mechanics by Rasikh Tariq

Thank you

22Department of Mechanical Engineering - Mohammad Ali Jinnah University, Islamabad Campus