Fluid Mechanics, Lecture Notes - Engineering - 3, Study notes of Mechanical Engineering

Flow, Pressure, Properties of Fluids, Fluids vs Solids, Statics, Hydrostatic pressure, Manometry management, Hydrostatic forces Continuity equation, bernoulli equation, momentum equation, Laminar and Trubulent Flow, Boundary Layer, Theory Dimensional analysis

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Unit 3: Fluid Dynamics
CIVE1400: Fluid Mechanics www.efm.leeds.ac.uk/CIVE/FluidLevel1 Lecture 8 98
CIVE1400: An Introduction to Fluid Mechanics
Unit 3: Fluid Dynamics
Dr P A Sleigh: [email protected]
Dr CJ Noakes: [email protected]
January 2008
Module web site: www.efm.leeds.ac.uk/CIVE/FluidsLevel1
Unit 1: Fluid Mechanics Basics 3 lectures
Flow
Pressure
Properties of Fluids
Fluids vs. Solids
Viscosity
Unit 2: Statics 3 lectures
Hydrostatic pressure
Manometry / Pressure measurement
Hydrostatic forces on submerged surfaces
Unit 3: Dynamics 7 lectures
The continuity equation.
The Bernoulli Equation.
Application of Bernoulli equation.
The momentum equation.
Application of momentum equation.
Unit 4: Effect of the boundary on flow 4 lectures
Laminar and turbulent flow
Boundary layer theory
An Intro to Dimensional analysis
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CIVE1400: An Introduction to Fluid Mechanics

Unit 3: Fluid Dynamics

Dr P A Sleigh: [email protected] Dr CJ Noakes: [email protected]

January 2008

Module web site: www.efm.leeds.ac.uk/CIVE/FluidsLevel

Unit 1: Fluid Mechanics Basics 3 lectures Flow Pressure Properties of Fluids Fluids vs. Solids Viscosity Unit 2: Statics 3 lectures Hydrostatic pressure Manometry / Pressure measurement Hydrostatic forces on submerged surfaces Unit 3: Dynamics 7 lectures The continuity equation. The Bernoulli Equation. Application of Bernoulli equation. The momentum equation. Application of momentum equation. Unit 4: Effect of the boundary on flow 4 lectures Laminar and turbulent flow Boundary layer theory An Intro to Dimensional analysis Similarity

Fluid Dynamics

Objectives

1.Identify differences between:

  • steady/unsteady
  • uniform/non-uniform
  • compressible/incompressible flow

2.Demonstrate streamlines and stream tubes

3.Introduce the Continuity principle

4.Derive the Bernoulli (energy) equation

5.Use the continuity equations to predict pressure and velocity in flowing fluids

6.Introduce the momentum equation for a fluid

7.Demonstrate use of the momentum equation to predict forces induced by flowing fluids

Flow Classification

Fluid flow may be classified under the following headings

_______________:

Flow conditions (velocity, pressure, cross-section or depth) are the same at every point in the fluid. _________________:_ Flow conditions are not the same at every point.

________________:

Flow conditions may differ from point to point but DO NOT change with time.

________________:

Flow conditions change with time at any point.

Fluid flowing under normal circumstances

  • a river for example - conditions vary from point to point we have non-uniform flow.

If the conditions at one point vary as time passes then we have unsteady flow.

Combining these four gives.

________________________. Conditions do not change with position in the stream or with time. E.g. flow of water in a pipe of constant diameter at constant velocity.


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


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


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

This course is restricted to Steady uniform flow

  • the most simple of the four.

One dimensional flow:

Conditions vary only _______________________ not across the cross-section.

The flow may be unsteady with the parameters varying in time but not across the cross-section. E.g. Flow in a pipe.

But:

Since flow must be zero at the pipe wall

  • yet non-zero in the centre - there is a difference of parameters across the cross-section.

Pipe Ideal flow Real flow

Should this be treated as two-dimensional flow? Possibly - but it is only necessary if very high accuracy is required.

Two-dimensional flow

Conditions vary in the direction of flow and in

___________________ at right angles to this.

Flow patterns in two-dimensional flow can be shown by curved lines on a plane.

Below shows flow pattern over a weir.

In this course we will be considering:




Some points about streamlines:

  • Close to a solid boundary, streamlines are _______________ to that boundary_
  • The direction of the streamline is the ________ of the fluid velocity
  • Fluid can not _______ a streamline
  • Streamlines can not cross ______________
  • Any particles starting on one streamline will stay on that same streamline
  • In __________ flow streamlines can change position with time
  • In _______ flow, the position of streamlines does not change.

Streamtubes

A circle of points in a flowing fluid each has a streamline passing through it.

These streamlines make a tube-like shape known as a streamtube

In a two-dimensional flow the streamtube is flat (in the plane of the paper):

Flow rate

Mass flow rate

m 

dm

dt

mass

time taken to accumulate this mass

Volume flow rate - Discharge.

More commonly we use volume flow rate Also know as discharge.

The symbol normally used for discharge is Q.

discharge, Q

volume of fluid

time

Discharge and mean velocity

Cross sectional area of a pipe is A Mean velocity is um.

Q = Au m

We usually drop the “m” and imply mean velocity.

Continuity

Mass entering = Mass leaving + Increase

per unit time per unit time of mass in

control vol per unit time

For steady flow there is no increase in the mass within the control volume, so

For steady flow

Mass entering = Mass leaving per unit time per unit time

Q 1 = Q 2 = A 1 u 1 = A 2 u (^2)

Mass flow in Cvolumeontrol

Mass flow out

In a real pipe (or any other vessel) we use the mean velocity and write

ρ 1 A 1 u m 1 = = =

For incompressible, fluid ρ 1 = ρ 2 = ρ

(dropping the m subscript)

This is the continuity equation most often used.

This equation is a very powerful tool. It will be used repeatedly throughout the rest of this course.

Some example applications of Continuity

  1. What is the outflow?
  2. What is the inflow?

Lecture 9: The Bernoulli Equation

Unit 3: Fluid Dynamics

The Bernoulli equation is a statement of the principle of conservation of energy along a streamline

It can be written:

p

g

u

g

1 1 z

2 1

+ + = H = Constant

These terms represent:

Pressure

energy per

unit weight

Kinetic

energy per

unit weight

Potential

energy per

unit weight

Total

energy per

unit weight

These term all have units of length,

they are often referred to as the following:

pressure head = velocity head =

potential head = total head =

Restrictions in application of Bernoulli’s equation:

  • Flow is _________
  • Density is __________ (incompressible)
  • ____________ losses are __________
  • It relates the states at two points along a single streamline, (not conditions on two different streamlines)

All these conditions are impossible to satisfy at any instant in time!

Fortunately, for many real situations where the conditions are approximately satisfied, the equation gives very good results.