1

DEPARTMENT OF MECHANICAL ENGINEERING

COLLEGE OF ENGINEERING

TENAGA NASIONAL UNIVERSITY

MALAYSIA

ENGINEERING MEASUREMENT

LAB. MANUAL

MESB 333

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Table of Contents

Laboratory Syllabus 3

Overview 4

Laboratory Time 5

Format for Logbook 6

Format for Formal Report 7

Lab No.1: Strain Measurement

Prelab Questions 9

Experiment I: Getting to know the equipment 10

Experiment II: The Bending System 16

Experiment III : The Torsion System

Experiment IV : The Tension System

Lab No. 2: Determining fluid (air) velocity and Discharge Coefficient

Prelab Questions 20

Experiment I: Velocity Measurement Using Pitot Tube 21

Experiment II: Determination of Discharge Coefficient 26

Lab No.3 Temperature Measurement

Prelab Questions 31

Experiment I: Time Constant 32

Experiment II: Type K Thermocouple 39

Experiment III: Humidity Measurement 42

Lab No.4 Photo Transducer

Prelab Questions 45

Experiment I: Photo Diode 51

Experiment II: Photo Conductive Cell 54

Experiment II: Photo Transistor 57

Lab No. 5 Flow Rate Measurement

Prelab Questions 60

Experiment: Flow Rate Measurement Devices 61

Lab No. 6 Introduction to PID Controller

Prelab Questions 66

Experiment: PID Controller 67

Lab No. 7 Free and Damped Vibration

Prelab Questions 66

Experiment I: Spring Coefficient (Stiffness) 67

Experiment II: Natural Frequency

Experiment III: Free and damped Vibration

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Laboratory Syllabus

Lab 1 : Strain Measurement

The experiments are related to the field of mechanics of deformable solid. The 1st experiment is on

bending of a cantilever beam. The 2nd experiment involves loading weighs on a circular bar to create

torsion. Strain gauge is used to convert the value of body deformation to corresponding electric signal

for analog reading. Simple calculation for strain is required using basic bending theory.

Informal report is required for this lab.

Lab 2 : Determining fluid (air) velocity and Discharge Coefficient

There are two experiments in this lab. These experiments are related to the field of Fluid Dynamics of

air. Both experiments use the same apparatus. 1st experiment is to measure air flow velocity. Pressure

along the test pipe will be measured to determine air flow velocity using Bernoulli’s equation. 2nd

experiment is to measure the discharge coefficient of an orifice plate and a nozzle. An orifice plate will

be inserted along the test pipe.

Formal report is required for this lab.

Lab 3 : Temperature Measurement

This experiment is related to the field of Heat Transfer and Thermodynamics. This experiment consists

of temperature measurement using different type of measuring devices: Pt 100 resistance thermometer,

liquid filled thermometer and NTC temperature probe etc. The apparatus consists of rice cooker, oven,

amplifier, and temperature indicator and so on connected in a simple circuit.

Understanding the working principle of resistance thermometer is important to students in order

to design their own procedures/steps to achieve the objectives and how to capture the results. The

student creativity and learning process in class is applied.

Formal report is required for this lab.

Lab 4 : Photo-electric Transducer

This lab is related to the field of physics, the behavior of light. Light intensity can be measured by

measuring the effect of the light on a device. When light falls on a material, current that corresponds to

the light intensity will be generated using transducer. Photocell, circuit box and light source are the

important devices in this experiment. The current that is produced at different level of light intensity

will be measured.

Informal report is required for this lab.

Lab 5 : Flow rate Measurement

This experiment is related to the field of fluid dynamics. This experiment involves the study of liquid

flow rate. Water is used as the fluid in this experiment. Three flow rate measurement devices: orifice

plate, variable area meter and venturi meter are used. The orifice plate and venturi meter require

calculation using Bernoulli equation to give the flow rate reading while variable area meter gives

reading directly Informal report is required for this lab.

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Lab 6 : Process Control Unit

This experiment is related to the field of Process Control. A system with different controllers will be

studied for it response to the controllers. The controllers are proportional controller, integrative

controller and derivative controller. The flow rate of water in a continuous loop is to be studied as a

system. This system is connected to computer software that enables the gain of each controller to be

set, and enables the result to be plotted. In this lab, the function of different controllers will be noticed.

The function of different controllers and working principle will be noticed by the students in

order to design their own procedures/steps to achieve the objectives and how to capture the

results. The student creativity is applied.

Informal report is required for this lab.

Lab 7. Vibration

In this lab, the students are to measure the stiffness of helical springs and its natural frequency. To

expose to free and damped vibration system with their characteristic that are related to the theory learn

in class.

LABORATORY & REPORTS: AN OVERVIEW

All experiments in the Engineering Measurements Laboratory require either a laboratory report

(Logbook) or a formal laboratory report for selective experiments, unless it is stated otherwise.

The reports should be simple and clearly written. Laboratory reports (logbook) are due after all

of the experiments are performed, unless it is stated otherwise. Final reports should be

submitted a week after the experiment’s day, unless it is stated otherwise. Any late submission

will not be entertained, unless there are concrete and unavoidable reasons.

The laboratory reports (log book) should be in hand writing and any graphs needed should be

drawn in either an appropriate graph paper or drawn using EXCEL, whichever suitable.

However, for final laboratory reports, it should be computer-generated and any graphs should

be drawn using EXCEL.

The formal laboratory reports should be submitted into pigeon hole in front the lab or to the

instructor directly.

The pre-lab questions in this lab manual should be answered and submitted during the first 5

minutes before you start your experiment accordingly.

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Laboratory Session

Lab Technician : Khairul Anwar Bin Derahman

Tel: 03- 8921 2020 ext. 6324

Laboratory Time:

Section 1A: Thursday - 1600-1900 (BL-0-003)

Section 1B: Friday - 800-1100 (BL-0-003)

Section 2A: Wednesday - 800-1100 (BL-0-003)

Section 2B: Tuesday - 900-1200 (BL-0-003)

Section 3A: Monday - 800-1100 (BL-0-003)

Section 3B: Tuesday - 1500-1800 (BL-0-003)

Attendance:

Please sign attendant sheet upon arrived to lab. Mark will be given depending on time of arrival. Student

who comes 15 minutes after the lab begins will get 0 mark. Absence due to illness should be proven by

medical certificates (MC).

Prelab:

Turn in prelab at the beginning of each lab. No prelab will be accepted 15 minutes after the lab begins.

Prelab will not be return to the students until the end of semester. The purpose of prelab is to encourage

student to read through lab manual before coming to the lab.

Logbook:

Students are required to prepare a logbook for the purpose of recording the data and discussing the

results from each informal experiment. The logbook MUST be presented to the instructor and signed at

the end of each laboratory session. Marks will be given for each experiment done in the session. Collect

the lab front page cover from the lab technician if you are assigned to write a formal report.

Laboratory Assessment:

Students are required to prepare a logbook for the purpose of recording the data and discussing the

results from each experiment. The logbook MUST be presented to the instructor and signed at the end

of each laboratory session. Marks will be given for each experiment done in the session. Collect the lab

front page cover from the lab technician if you are assigned to write a formal report.

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Formal Reports:

There are a total of 2 individual formal reports that need to be completed by each student throughout

the course. The formal reports should be written for the following experiments.

Experiment 2: Determining fluid (air) velocity and Discharge Coefficient. – Group Report -5%

Experiment 1: Temperature Measurement.- Individual Report – 7%

Duration of one-week period is provided for formal report and should be submitted during the next lab.

Report should be submitted to the lab technician personally. Grade will be deducted from the late report

as follows (except with valid reason) : Late submission penalty : Late 1 day : 90%, Late 2 days : 80

%, Late 3 days : 70%, More than 3 days: 50% of earned mark.

Plagiarism is not acceptable. It will result in half of the total grade being deducted or zero grade for

the lab report or for the whole course. In addition, poor report writing will result in meeting the

instructor for improvement in future report writing. Please use the font of Arial or Times New Roman

only.

Before submitting your hardcopy formal report to the instructor, you need to upload your

softcopy report into TURNITIN program, to check for similarity (report with silmilarity higher

than 50% will not be accepted). You will be given ID and password to upload the softcopy of your

formal report by the respective instructors.

Experiment Group:

Students will perform experiment in-group. Each experiment group consists of 3-5 students.

Group number consists of Section number, follows with number appointed. For example, the first

group from section 1A will have group number of 1A1; the second group in the same section will be

designated as 1A2 and so on.

Report must be submitted using front page supplied.

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Format for LOGBOOK

No. Criteria

1 Title Page

With name, SID, group no., lab no., date performed, date submitted.

2 Statement of Purpose or Objective

With clear, specific purpose statement

3 Data, Observation and Results

With results clearly, orderly presented in either graph, spreadsheet, table etc with

labeled. Sample calculation if calculation is involved. Error calculation

4 Analysis and Discussion

With specific comment, explanation, support on the results based on theory. Error

and uncertainty analysis ie. Error source, comparison between the experimental

and theoretical results. Answer to question if given.

5 Conclusion

Summary of the experiment. Conclusion drawn from results in the light of the

stated objective.

6 Overall report presentation

Neat, Clear label of small title etc. With references if given

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Format for Formal Report

General Instructions:

Font type: Arial or Time New Roman Paper size: A4

Font size: 12 pt Ink colour: black

Spacing: 1.5 Graph: computer generate

No. Criteria

1 Title Page

With name, SID, group no., lab no., date performed, date submitted.

2 Table of Content

3 Summary/Abstract

The concise overview of the report.

4 Statement of Purpose or Objective

A brief description of what the experiment is demonstrating.

5 Theory

With brief but clear background and theory related to the experiment.

6 Equipment

Diagram of the apparatus and specification.

7 Procedure

A step by step explanation of what was done in the lab and why each step was

performed.

8 Data, Observation and Results

With results clearly, orderly presented in either graph, spreadsheet, table etc

with labeled. Sample calculation if calculation is involved. Error calculation

9 Analysis and Discussion

With specific comment, explanation, support on the results based on theory.

Error and uncertainty analysis ie. Error source, comparison between the

experimental and theoretical results. Answer to question if given.

10 Conclusion

Summary of the experiment. Conclusion drawn from results in the light of the

stated objective.

11 Overall report presentation

Neat, Clear label of small title etc. With references if given

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MESB 333 LAB NO.1 :

STRAIN MEASUREMENT

PRELAB QUESTIONS

Name: ________________________SID: ______________Group:______ Date:_______________

1. What is stress? Strain? What is the relationship between stress and strain?

2. What is the principle used in strain gauge measurements?

3. What is the different between quarter, half and full bridge?

4. How to eliminate error due to temperature changes?

5. In measuring the torsion strain, how can the axial or bending strain be eliminated? Sketch to

explain.

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MESB 333 Lab No.1

Strain Measurement

____________________________________________________________________________

1. Theory

A material will be deformed to certain extend when external forces act on it. This deformation

will cause changes in length and diameter of the material. The strain produced is directly

proportional to the stress at a limited region, which is called the limit of proportionality (i.e. there

is linear relation between the two). The stress-strain graph is a straight line in this region. In this

experiment, we are going to study the performance of an electrical resistance strain gauge as well

as to verify its accuracy on measuring the strain of a bending material.

Hooke's Law, which relates stress and strain, can be applied in the limit of proportionality

region. Young's Modulus of Elasticity is the gradient of straight line in the stress-strain graph. The

mathematical relationship is:

EEA

P

L

dL …………………………………………(1)

where,

dL : change in length L

: strain

P : force on cross section area A

E : Young’s Modulus of Elasticity

: axial stress

Equipment used to measure dL is called extensometer. It is a mechanical method to measure

dL where change in length can be magnified. However, a better way to measure dL is by using the

electronic measurement. Longitudinal strain is associated to the changes in length of a material.

While diametral strain is associated to the changes in the diameter of a material. Poisson's ratio is

the ratio of longitudinal strain to diametral strain or can be given as

Poisson’s ratio() = lateral contraction per unit breadth

Longitudinal extension per unit length

When the length and the diameter of a material change, the electrical resistance of the material

will change too. The relationship between the change in the dimension to the electrical resistance

of the material can be related mathematically as equation shown:

A

LR

……………………………………………..(2)

where,

R : electrical resistance

: specific resistance of material

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L : length

A : cross sectional area

From the relationship, it is clear that the resistance will increase when the material is

stretched. Conversely, compression will cause the resistance to decrease. Strain gauge uses

this principle to measure the strain.

2. Calculation of axial strain

Theoretically, the strain value can be calculated using the theory of bending at the

point of attachment of the strain gauge. For a rectangular cross-sectional area cantilever beam,

………………………………..(3)

Where,

M : bending moment = (Applied load X moment arm)

I : second moment of area of cantilever = 12

bd3

(Width b and thickness d)

: axial stress

y : half the thickness of the cantilever = ½ d

E : modulus of elasticity

R : radius of curvature of cantilever due to M

Strain is defined as change in length per unit length, that is

……………………………………………………………….(4)

From the theory of bending

……………………………………………………………….(5)

Hence, the theoretical strain value is

……………………………………………………………(6)

I

My

R

E

yI

M

R

y

L

dL

EI

M

R

1

EI

My

R

y

12

From the dimension of cantilever beam, M = 420* Load (N.mm)

*420 mm is the distance from the load point to strain gauge.

Measurement of the resistance is usually done using the Wheatstone Bridge. The gauge is

attached to the material using a high-grade adhesive. Since temperature will affect the resistance,

this factor must be taken into consideration too

Having studied the use of a strain gauge for measuring tensile(axial) strain and stress,

a more complicated application can now be considered. Reverting to the diagram of

the standard bridge there are further ways of exploiting the measuring technique. In

this experiment, we are going to study the measurement of torsion strain.

Suppose the temperature compensation gauge used as R, can be attached to the structural element

being tested in such a way it is subjected to an equal but opposite strain to the R, gauge. This will double

the meter reading while providing the temperature compensation and is known as reversed active strain

gauging. This could have been done in the case of bending by attaching a strain gauge on the underside

of the cantilever where the compression due to bending equals the tension where the top surface gauge

is fixed. The leads from the underside gauge would then replace the leads from the dummy gauge. Now

consider a hollow round tube used as a cantilever.

Figure 3. Cantilever round bar exert with torsion.

In bending there is a neutral axis at the horizontal axis, so any gauge fixed

symmetrically about this neutral axis will not record a strain, By applying torque at the free

end of the cantilever, a uniform shear is induced along the whole length. This in turn

produces diagonal tension and compression stresses of equal value along the

corresponding 450 helical directions. Hence by fixing two strain gauges at A and B as

shown the following conditions are satisfied:

(1) Temperature compensation

(2) Net axial strain effect is zero for either A or B

(3) Gauge A is subjected to diagonal tension while gauge B is in diagonal

compression, or vice versa.

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The meter will therefore indicate twice the diagonal strain from which the stress can

be derived using the modulus of elasticity.

2.3 Calculation of torsion strain

Hooke’s Law

……………………………………………………..(7)

For the torsion specimen the comparable theoretical equation is

J

Tr

L

G

rJ

T

……………………………………..(8)

where

T : torsion = (Applied Load X eccentricity)

J : polar moment of inertia of tube = 4

1

4

o DD32

Do : outside diameter

Di : inside diameter

: surface shear stress

r : outside radius of tube

G : modulus of rigidity

: angular twist over length L

The shear stress acts circumferentially and has to be accompanied by a system of

complementary stresses including diagonal tensile and compressive stresses, which are

E

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perpendicular to each other. Hence there are equal direct strains along opposing 450

helices on the surface of the tube given by

EJ

Tr

E

q

……………………………………(9)

and the meter will indicate 2*.

3 Wheatstone Bridge

Figure 1 Wheatstone bridge

R1 will be the strain gauge attached to the material. It is also called an active gauge. R2 is a similar

strain gauge to R1. But, it is attached to an unstressed part of the material. The effect of temperature

on R1 and R2 will be similar. R3 and R4 are high stability resistors of equal value.

M is a digital voltmeter or a purpose designed high stability high gain amplifier with a digital

meter and a zeroing circuit. Voltage applied to A and C is a constant DC voltage. Normally it is 1-

2 volts. External zeroing is applied in Wheatstone Bridge. External zeroing means the meter M will

show zero reading. This is done by having a variable resistor at D. Zeroing can be done by varying

the variable resistor. Zeroing is required because factor like weight of the material can affect the

results.

Refer to the strain gauge trainer manual in the moodle for more detail

how to perform this experiments.

B

R1 R2

A M C

+ _

R3 R4

D

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MESB 333 LAB NO. 2:

VELOCITY MEASUREMENT

AND DETERMINATION OF DISCHARGE COEFFICIENT

PRELAB QUESTIONS

Name: _____________________SID: ______________ Group:______ Date:______________

1. Draw a diagram and explain briefly how to measure pressure using pitot tube?

2. What is coefficient of discharge?

3. What is Reynolds number?

4. Describe three different flow characteristics and what determines each characteristic?

5. What is orifice plate is use for ? Gives 2 examples UNITS for measuring flowrate?

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MESB 333 Lab No.2

Determining fluid(air) velocity and Discharge Coefficient

1. Experiment I

Velocity Measurement Using Pitot Tube

1.1. Objective

This experiment allows student to learn the method of measuring air flow velocity using pitot

tube. The student will understand the working principle of pitot tube as well as the importance of

Bernoulli equation in deriving and calculating the velocity.

1.2. Theory

A pitot tube is used to explore the developing boundary layer in the entry length of a pipe which

has air drawn through it. With pitot tube, the velocity distribution profiles can be determined at a

number of cross-sections at different locations along a pipe. With pitot tube, air flow velocities in

the pipe can be obtained by first measuring the pressure difference of the moving air in the pipe at

two points, where one of the points is at static velocity. The Bernoulli equation is then applied to

calculate the velocity from the pressure difference.

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ghorp

v

(1)

p The pressure difference between the pitot tube and the wall pressure tapping measured using

manometer bank provided (gx where x is the level of fluid used in the manometer).

h’ The pressure difference expressed as a 'head' of the fluid being measured (air)

The air density at the atmospheric pressure and temperture of that day.(kg/m3)

g gravitational acceleration constant (9.81 m/s2)

When fluid flows past a stationary solid wall, the shear stress set up close to this boundary due to

the relative motion between the fluid and the wall leads to the development of a flow boundary

layer. The boundary layer may be either laminar or turbulent in nature depending on the flow

Reynolds number.

The growth of this boundary layer can be revealed by studying the velocity profiles at selected

cross-sections, the core region still outside the boundary layer showing up as an area of more or

less uniform velocity.

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If velocity profiles for cross-sections different distances from the pipe entrance are compared, the

rate of growth of the boundary layer along the pipe length can be determined. Once the boundary

layer has grown to the point where it fills the whole pipe cross-section this is termed "fully

developed pipe flow".

1.3. Reynolds Number

The Reynolds number is a measure of the way in which a moving fluid encounters an obstacle. It's

proportional to the fluid's density, the size of the obstacle, and the fluid's speed, and inversely

proportional to the fluid's viscosity (viscosity is the measure of a fluid's "thickness"--for example,

honey has a much larger viscosity than water does).

vdRe

fluid density

v : fluid velocity

d : obstacle size

coefficient of fluid dynamic viscosity

A small Reynolds number refers to a flow in which the fluid has a low density so that it responds

easily to forces, encounters a small obstacle, moves slowly, or has a large viscosity to keep it

organized. In such a situation, the fluid is able to get around the obstacle smoothly in what is known

as "laminar flow." You can describe such laminar flow as dominated by the fluid's viscosity--it's

tendency to move smoothly together as a cohesive material.

A large Reynolds number refers to a flow in which the fluid has a large density so that it doesn't

respond easily to forces, encounters a large obstacle, moves rapidly, or has too small a viscosity

to keep it organized. In such a situation, the fluid can't get around the obstacle without breaking

up into turbulent swirls and eddies. You can describe such turbulent flow as dominated by the

fluid's inertia--the tendency of each portion of fluid to follow a path determined by its own

momentum.

The transition from laminar to turbulent flow, critcal flow, occurs at a particular range of

Reynolds number (usually around 2500). Below this range, the flow is normally laminar; above it,

the flow is normally turbulent.

1.4. Calculation of air flow velocity

The manometer tube liquid levels must be used to calculate pressure differences, h and pressure

heads in all these experiments. Starting with the basic equation of hydrostatics:

p = gh (2)

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we can follow this procedure through using the following definitions:

Example:

Manometer tubes 1(static ‘pressure’*) 2(stagnation ‘pressure’)

Liquid surface readings

(mm)

X1 X2

Angle of inclination, = 0

‘pressure’ term is used since this reading is in mm of manometer fluid and not the pressure of unit

Pa.

Therefore the equivalent vertical separation of liquid levels in manometer tubes,

h = (x1 - x2)cos (3)

If k is the density of the kerosene in the manometer, the equivalent pressure difference p is:

p = k gh = k g(x1 - x2) cos (4)

The value for kerosene is k = 787 kg/m3 and g = 9.81 m/s2. If x1 and x2 are read in mm, then:

p = 7.72(x1 - x2)cos [N/m2] (5)

The p obtained is then used in second equation (1) to obtain the velocity.

To use the first equation (1), convert this into a 'head' of air, h’. Assuming a value of 1.2 kg/m3 for

this gives:

cos.

1000

)(.' 21 xx

hair

k [N/m2] (6)

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1.5 Apparatus

Figure 1 Experiment apparatus

1.6 Procedure

a) Five mounting positions are provided for the pitot tube assembly. These are: 54 mm, 294 mm,

774 mm, 1574 mm and 2534 mm from the pipe inlet

b) Ensure that the standard inlet nozzle is fitted for this experiment and that the orifice plate is

removed from the pipe break line.

c) Set the manometer such that the inclined position is at 00.

d) Mount the pitot tube assembly at position 1 (at 54mm, nearest to the pipe inlet). Note that the

connecting tube, the pressure tapping at the outer end of the assembly, is connected to a

convenient manometer tube. Make sure that the tip, the L-shape metal tube of the pitot tube

is facing the incoming flow.

e) Note that there is a pipe wall static pressure tapping near to the position where the pitot tube

assembly is placed. The static pressure tapping is connected to a manometer tube.

f) Position the pitot tube with the traverse poisition of 0mm. Start the fan with the outlet throttle

opened.

g) Starting with the traverse position at 0mm, where the tip is touching the bottom of the pipe,

read and record both manometer tube levels of the wall static and the pitot tube until the

traveverse position touching the top of the pipe.

h) Repeat the velocity traverse for the same air flow value at the next positon with the pitot tube

assembly. Make sure that the blanking plugs is placed at the holes that are not in use.

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1.7 Results

Data Sheet for Velocity Measurement Using Pitot Tube

Traverse

Position

(mm)

Pitot Tube at 54 mm

Static 'Pressure' Reading

____________(mm)

Pitot Tube at 294 mm

Static 'Pressure' Reading

____________(mm)

Stagnation

'Pressure'

Reading

(mm)

x

(mm)

p

(N/m2)

velocity

(m/s)

Stagnation

'Pressure'

Reading

(mm)

x

(mm)

p

(N/m2)

Velocity

(m/s)

0

10

20

30

40

50

60

70

80

Traverse

Position

(mm)

Pitot Tube at 774 mm

Static 'Pressure' Reading

____________(mm)

Pitot Tube at 1574 mm

Static 'Pressure' Reading

____________(mm)

Stagnation

'Pressure'

Reading

(mm)

x

(mm)

p

(N/m2)

velocity

(m/s)

Stagnation

'Pressure'

Reading

(mm)

x

(mm)

p

(N/m2)

Velocity

(m/s)

0

10

20

30

40

50

60

70

80

21

Pitot Tube at 2534 mm

Static 'Pressure' Reading ____________(mm)

Traverse

Position

(mm)

Stagnation

'Pressure'

Reading(mm)

x

(mm)

p

(N/m2)

velocity

(m/s)

0

10

20

30

40

50

60

70

80

Calculate air velocity at each point using equations (1), (5) or (6).

Plot the traverse velocity profiles in one graph (Velocity against traverse position). Note

that the boundary layer grows in the pipe to fill the whole cross-section; fully developed

pipe flow most likely occurred by the third or fourth position.

Give your comments on the velocity profiles.

Include error analysis.

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2 Experiment II

Determination of Discharge Coefficient

2.1 Objective

This experiment will ask student to determine the discharge coefficients, CD for orifice plate and

the small nozzle.

2.2 Introduction

An orifice plate meter forms an accurate and inexpensive device for measuring the discharge

for the flow of liquids or gases through a pipe. The orifice provided can be inserted into the

suction pipe at the flanged joint approximately half way along its length. The multi-tube

manometer provided is used to measure the pressure drop across the orifice and this is related to

the discharge determined independently.

In this experiment, we are going to determine the discharge coefficient experimentally for an

orifice plate in an airflow pipe. Also using the static pressure tapings provided, we are

determining the pressure distribution along the pipe downstream of the orifice plate. From the

obtained CD of the orifice plate, we will determine the CD of a small nozzle.

2.3 Theory

The orifice plate meter forms a jet, which expands to fill the whole pipe, some diameter

distance downstream. The pressure difference between the two sides of the plate is related to the

jet velocity, and therefore the discharge, by the energy equation:

where Q = discharge (volume/time)

Aj = jet cross-section area at minimum contraction (vena contracta)

Ao = orifice cross- 2/4: d = orifice size)

vj = jet velocity at minimum contraction (vena contracta)

Cc = coefficient of contraction of jet

Cv = coefficient of velocity of jet

g = gravitational acceleration (9.81 ms -2)

h = pressure difference 'head' of air across orifice (refer to equation (6) of Exp. I)

These two coefficients are normally combined to give a single coefficient of discharge: CD = Cc.Cv

Equation (1) now becomes

(2)

If Q can be determined independently, then the discharge coefficient can be determined as follows:-

Values of Qi can be determined if the standard nozzle is fitted at the pipe inlet.

(3)

(4)

2ghv

Cc

Co

A j

vc

Co

A j

vj

A Q

gh2A

QC

o

D

ghAo 2CQ D

iD'

ii gh2CAQ

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If hi = the drop in pressure head across the inlet, the discharge = (k/air )* (xbefore nozzle –xafter nozzle):

in which Ai = standard nozzle cross-section area (= d2 /4) and C’D assumed to be 0.97. Values of

h I are obtained from the manometer tube levels connected to the pipe inlet pressure tapping and

open to the atmosphere.

2.4 Calculating the CD of orifice plate:

From equation (4), with the Qi obtained from standard nozzle where CD of standard nozzle is

assumed to be 0.97, we can calculate the CD of orifice plate. Assuming that Qi across standard

nozzle and Qo across orifice plate is the same, apply equation (3)

……………………………(5)

Where ho = (k/air)*(x across orifice)

Ao = cross section area of orifice plate hole

2.5 Apparatus

Figure 2 Experiment Diagram

2.6 Procedure

(a) Insert the orifice plate in position (taking care to observe the instructions as to) in which the

surface should face the approaching airflow.

(b) Connect all the static pressure tapping points to the manometer tubes ensuring that one

manometer tube remains unconnected to record room air pressure and that one is attached to

the first tapping point adjacent to the standard inlet nozzle which should be fitted.

(c) Turn on fan with low airflow (damper plate closed) and read all manometer tubes, including

any open to the air (reading should be taken after the fan is on).

(d) Gradually increase air flow by increasing the damper opening to 100%, and take read at all

opening.

oo

oD

ghA

QC

2

24

Measure the diameter of the orifice plate, and the pipe for computing the cross sectional area

and Reynolds number.

2.7 Results

Table 5.1 Static ‘Pressure’ Readings when using Standard Nozzle (80 mm)

Damper Openings (% Openings)

0% 25% 50% 75% 100%

Points mm of kerosene

Room

“pressure”

After nozzle

54mm

294mm

774mm

Before

Orifice

After Orifice

1574mm

2534mm

Table 5.2 Static ‘Pressure’ Readings when using Small Nozzle (50 mm)

Damper Openings (% Openings)

0% 25% 50% 75% 100%

Points mm of kerosene

Room

“pressure”

After nozzle

54mm

294mm

774mm

Before

Orifice

After Orifice

1574mm

2534mm

25

From table 5.1using equation (4) calculate the Qi, then using equation (3) where Q=Qi

calculate the CD for orifice plate for each damper opening.

For data in table 5.2, using similar procedures, but this time using the value of CD for orifice

found previously, you need to calculate the CD for small orifice for each damper opening.

For each case, plot values of CD obtained against corresponding values of Reynolds number

(Re) obtained using the relationship:

……………………………………..(6)

where : the coefficient of dynamic viscosity of the air air density

v : is the mean pipe velocity (Qi/Ap)

d : the pipe diameter.

Also plot longitudinal pressure profiles for both tables from the manometer readings.

(mm kerosene against tapping position)

Discuss what happen as the air flow past through the orifice plate.

Discuss the CD obtained for orifice and small nozzle.

What happen to the CD when you increase the damper opening?

What happen to the manometer reading when the damper opening changes. Discuss.

Any obstruction such as an orifice plate would actually cause a pressure drop but by

analyzing the graph below or from your data you should see that the reading in mm of

kerosene is increased. Explain.

Air Flow

vdRe

mm

Kero

sen

e

Tapping position along test pipe

Pressure Drop across Orifice Plate

26

MESB 333 LAB NO. 3 TEMPERATURE MEASUREMENT

PRELAB QUESTIONS

Name: _____________________SID: ______________ Group:______ Date:______________

1. Describe the working principle of a thermistor and resistance thermometer. What are the differences?

2. What is time constant?

3. What are the materials commonly used for resistance thermometer?

i) ________________________________________ ii) ________________________________________ iii) _________________________________________

4. Gives two examples where PTC thermistors are generally used?

i) ________________________________________ ii) _______________________________________

27

MESB 333 Lab No. 3

Temperature Measurement

______________________________________________________

1 Experiment I

Time Constant

1.1 Objective

Design your experiment in order:

1. To compare the time constant of different type of temperature measuring devices with

reference to mercury filled thermometer (smallest time constant).

2. To understand the relationship between resistance and temperature.

1.3 Theory

Temperature is a measure of hotness. Together with a measure of ‘thermal mass’ of a body it

gives an indication of the total thermodynamics energy that body contains. There are many scales

for the comparison of temperatures, the most important is with their corresponding values for

melting ice and boiling water (which are common reference temperatures) being given in the

table below.

Scale Melting Ice Boiling Water

Celsius (or Centigrade) 0 0C 100 0C

Fahrenheit 32 0F 212 0F

Kelvin (Absolute Scale) 273 K 373 K

In this experiment you will be familiarized with the following temperature measurement devices:

a) Resistance thermometer (TYPE K)

b) Thermistor (NTC)

1.4 The Liquid Filled Thermometer

This type of thermometer depends on the expansion of a liquid associated with an increase in

temperature. The most common type is the mercury-in-glass thermo meter. This thermometer

consists of a capillary tube with a bulbous end . clean , dry mercury is introduced and the

28

thermometer heated to drive off the air. The end is then scaled leaving mercury and mercury

vapour only.

On heating, the mercury expands relative to the glass container and a column is pushed along the

bore of the tube. A scale along the tube, calibrated in units of temperature, gives a direct reading

of temperature. The mercury-in-glass thermometer is an accurate device but is very fragile and

care should be exercised in use. This type of thermometer should not be used in applications such

as the food industry where mercury poisoning could occur in the event of breakage.

The mercury may be replaced by other fluids according to the application. For example, alcohol

is cheaper and may be used at lower temperatures than mercury. A mercury-in-glass thermometer

is supplied with the Temperature Measurement Bench due to its stable and accurate performance.

For accurate measurement of temperature using a liquid filled thermo meter, it is important that

the thermometer is immersed into the medium being measured by the correct amount. The depth

of immersion is usually stated on the stem of the thermo meter and defines the condition under

which calibration is maintained. The immersion depth may be partial or total and is independent

of filling or range

1.5 The Vapor Pressure Manometer

For industrial applications, the liquid-in-glass thermometer is far from suitable due to its fragility

and the difficulty in reading. In these applications the glass is replaced by a metal container and

mechanical indication is substituted. One example of this type of thermo meter is the vapor

pressure thermo meter.

This consists of a metal bulb partially filled with fluid, which is connected to the sensing element

of a Bourdon gauge. The space above the fluid is filled with vapor of the fluid, the pressure of

which is display on the Bourdon gauge. The gauge is calibrated directly in units of temperature

corresponding to the equivalent, pressure of the vapor but calibration is far from linear due to the

pressure increasing more and more rapidly as the temperature increases. For this reason, the vapor

pressure thermometer is suitable only for operation over short ranges of temperature and suffers

from lack of sensitivity at low readings. In service, the range should be selected so that the gauge

remains within operational limits with the normal operating point at approximately two thirds of

fullscale reading.

Vapor pressure thermometers offer the advantage of remote reading. The thermometer may be

ordered with a metal capillary tube connecting the bulb to the gauge, permitting remote operation

over distances up to sixty meters. Correct orientation of the bulb and gauge should be preserved

f or ac- curate results. The vapor pressure thermometer supplied with the bench has the Bourdon

gauge connected directly to the stem f or case of operation

1.6 The Bi-Metal Thermometer

Expansion of solids may be used to measure temperature but direct measurement is impractical due to the very small movements involved. However, if two thin met al strips, having d if f erent coeff icients of linear expression, are mechanically fastened together, the result is a strip which bends significantly when heated. This combination is called a Bi-metal strip and the sensitivity may be increased by coiling the strip into a spiral. One end of the strip is f ixed to the case and a pointer is attached to the other end. L inear scale may be obtain ed by suitable cho ice

29

of metals.

This type of thermometer is very robust and has many applications throughout industry where accuracy of measurement is not imp ortant.

The bi- metal thermometer supplied w ith the bench is mounted on th e back-board and gives a direct reading of ambient air temperature.

1.7 Resistance Thermometer

The resistance of a material changes with temperature. Resistance thermometer uses this

relationship in measuring the temperature. If high accuracy is required, the material used in

resistance thermometer is platinum. Nickel is used in general operation and monitoring. Copper

is also suitable but only in a restricted temperature range of approximately 250oC, because copper

tends to corrode more severely when subjected to oxidation.

Figure 3.1 shows the resistance change of the metals as a function of the temperature T. They

have a positive temperature coefficient . For the purpose of comparison a resistance

characteristics of a thermistor (NTC) was added, which runs much more non-linearly, and in

contrast to the metals, demonstrates a negative coefficient .

For small temperature ranges we may assume that linear relationships exist between resistance

and temperature. From figure 3.2 one can deduce the temperature-dependent resistance ratio

R(T) caused by the resistance change R is:

R(T) = Ro + R (1)

The rise of this function is m = R/T.

R = mT (2)

Knowing that, R(T) = Ro + R, thus:

R(T) = Ro + mT

= Ro (1 + m/Ro T)

= Ro (1 + T

R/R o

T) (3)

= Ro (1 + 1T) where, 1 = T

R/R o

30

Figure 3.1

1 is the linear temperature coefficient of the resistive material. It provides the relative change in

resistance (R/ Ro) for a certain temperature change (T), for example 0.4% change in resistance

per degree.

Figure 3.2

From Figure 3.1 we can see that for large measurement ranges no linear relationship between

resistance R and temperature T can be assumed. In this case we must take into consideration,

apart from the linear temperature coefficient 1 , also the square temperature coefficients 2, and

for very large temperature changes T also the cubic temperature coefficients 3, and if

necessary the biquadratic value 4.

nn2

21o T...TT1R)T(R (4)

where, oTTT

0

50

100

150

200

250

300

350

400

450

-200 0 200 400 600 800 1000

R/W

T/0C

Ni 100 Pt100

Cu100

R(T)

R Ro = R(To)

31

1.8 Thermal Response

The thermal response of a thermo meter to changes in te mperature is probably the most important characteristic to consider when selecting instrumentat ion f or a particular application.

A thermo meter may be extremely accurate and stable in performance but totally unsuitab le f or use in a dynamic situation, due to a time lag between system temperature and thermometer reading.

The d iagra m below shows typical response curves f or a thermo meter when step changes in

temperature are applied .

The response of the thermo meter is def ined by the t ime ta ken f or the te mperature reading to change by 63.2% of the step change. For any thermometer, this time will be a constant value irrespective of step change and is def ined as the "t ime constant" f or the thermometer. Th e time constant and response profile f or a thermometer will change if the system is modif ied. For example, t he speed of response of a thermometer will be slowed down if it is protected from the system being measured by a ther mo meter. The response will also be af fected by the thermal contact between the thermometer and pocket, f luid f illing of the pocket resulting in a reduction in time constant.

The response of the thermometer is def ined by the t ime taken f or the te mperature reading to change by 63.2% of the step change. For any thermometer, this time will be a constant value irrespective of step change and is def ined as the "time constant" f or the thermo meter. Th e time constant and re- sponse prof ile for a thermometer will change if the system is modified. For example, the speed of response of a thermometer will be slowed down if it is protected from the system being m easured by a thermometer. The response will also be af f ected by the thermal contact between the thermometer and pocket, f luid f illing of the pocket resulting in a reduction in time constant.

32

Figure 3.3 Experiment apparatus

setup

33

1.9 Apparatus Setup

Note: To discharge the hot water from the pot, request assistant from lab technician.

Base on Figure 3.3, construct the experiment procedure in order to achieve the objective.

34

2 Experiment II

Type K thermocouple

2.1 Objective

Design the experiment in order:

- To investigate the working principle of Type K Thermocouple - To find the sensitivity of the type K thermocouple - To investigate the relation between voltage output and temperature

2.2 Thermistor

Thermistors consist of semi-conducting polycrystalline material. In the production of

temperature sensors copper dioxide (CuO2) is preferred. It demonstrates a sever (non-linear)

drop in resistance for an increase in temperature. It possesses a negative temperature coefficient,

which is the reason why these sensors are called NTC resistors.

If the CuO2 is mixed with the ingredients of a ferroelectric material (e.g. BaTi), the

temperature coefficient is initially negative only for low temperatures. After reaching a threshold

temperature the temperature coefficient becomes very strongly positive in a narrow temperature

range. For even higher temperatures the temperature coefficient reverts back to negative.

Because of the clearly delineated positive temperature coefficient range, these sensors are called

PTC resistors. They are mainly used for trigger purposes.

2.3 Features of NTC and PTC thermistors

NTC sensors possess a high sensitivity, which is easily 10 times higher than that of metal

resistance thermometers. The non-linearity of NTCs and their broad manufacturers' tolerances

exclude them from use for precision instruments. In the temperature range between -60oC and

+150oC they are frequently used in the area of household appliances and medical technology

because of their high sensitivity and corresponding simple circuitry.

The effect of NTCs, whereby the resistance lowers as the temperature increases, is

explained by the semiconductor mechanism. In semi-conductors (as opposed to metal

conductors) the valency electrons have relatively strong bonds to the atomic nuclei of the crystal

lattice. A rise in temperature loosens this bond and more and more electrons enter into the

conduction band, where they are available for charge transport (i.e. for increased current), thus

reducing the ohmic resistance.

PTCs behave in the same manner below the threshold temperature. The resistance

lies only somewhat higher than for NTCs, because, due to the mixture of a ferroelectric

material to the semiconductor material an additional resistance of both components

results (series connection). However, with increasing temperature a strong increase in

resistance is observed within a narrow temperature range, which is caused so rapidly by

the sudden cancelling of a uniform orientation of all magnetic forces in the ferroelectric

35

material. Through thermal motion an amorphous crystal structure is produced, which

results in a considerable prolongation of the current paths, on which the electrons move

through the PTC. If this transition is completed, the resistance then drops again as the

rise in temperature continues. Thus the function R(T) of the PTC follows the

characteristic of its semiconductor components, supplemented by the characteristics of

its ferroelectric components.

They are generally intended for applications where a considerable change of

esistance is required as a function of themperature, or of dissipated power, for example:

heating elements, temperature indication, control or alarm, time-delay of relays, circuit

protection etc.

2.4 Temperature function and temperature coefficient of NTC thermometers

The resistance R(T) = RT of NTC materials can be described as a function of the

temperature using the following equation:

RT = AeB/T (5)

The material constant B is given in Kelvin, e.g. B = 3800 K. The constant A gives the

resistance for infinitely high temperature. As the sensor cannot register this temperature,

the constant A cannot be used as a practical parameter. The requirements for practical

application can be better satisfied with the following dependency RT. For this the

reference temperature To = 20oC is used, for which the resistance has its nominal value

Ro. Due to the fact that in the above equation only A is unknown, the equation is then

solved for A, which is inserted into RT:

R(To) = Ro = AeB/To

A = Roe-B/To (6)

Subsitute (6)into equation (5)

RT = RoeB(1/T - 1/To) (7)

Construct the experiment procedure in order to achieve the objective.

36

3 Experiment III

Humidity

3.1 Objective

Design the experiment in order:

- Understanding of whirling pyschorometer (hygrometer)

- Understanding of wet and dry bulb thermometer

- Measurement of ambient humidity using dry and wet bulb.

- 3.2 Introduction

Humidity is the amount of water vapor in the air. Relative humidity is defined as the ratio of the

partial pressure of water vapor in a parcel of air to the saturated vapor pressure of water vapor at

a prescribed temperature. Humidity may also be expressed as specific humidity. Relative

humidity is an important metric used in forecasting weather. Humidity indicates the likelihood of

precipitation, dew, or fog. High humidity makes people feel hotter outside in the summer because

it reduces the effectiveness of sweating to cool the body by reducing the evaporation of

perspiration from the skin. This effect is calculated in a heat index table

Hygrometers are instruments used for measuring humidity. A simple form of a hygrometer is

specifically known as a psychrometer and consists of two thermometers, one of which includes

a dry bulb and the other of which includes a bulb that is kept wet to measure wet-bulb

temperature. Modern electronic devices use temperature of condensation, changes in electrical

resistance, and changes in electrical capacitance to measure humidity changes. Hygrometers

measure humidity while psycrometers measure realative humidity in the air.

In a psychrometer, there are two thermometers, one with a dry bulb and the other with a wet bulb.

Evaporation from the wet bulb lowers the temperature, so that the wet-bulb thermometer usually

shows a lower temperature than that of the dry-bulb thermometer, which measures dry-bulb

temperature. When the air temperature is below freezing, however, the wet bulb is covered with

a thin coating of ice and yet may be warmer than the dry bulb. Relative humidity is computed

from the ambient temperature as shown by the dry-bulb thermometer and the difference in

temperatures as shown by the wet-bulb and dry-bulb thermometers. Relative humidity can also

be determined by locating the intersection of the wet- and dry-bulb temperatures on a

psychrometric chart. One device that uses the wet/dry bulb method is the sling psychrometer,

where the thermometers are attached to a handle or length of rope and spun around in the air for

a few minutes.

37

Your are given a whirling hygrometer for humidity measurement apparatus, write down the

procedure to achieve the objectives and to measure the Humidity of the Engineering

Measurement Lab.

Figure 3.3 Whirling hygrometer

38

MESB 333 LAB NO. 4 : PHOTO ELECTRIC TRANSDUCER

PRELAB QUESTIONS

Name: _____________________SID: ______________ Group:______ Date_______________

1. How to measure the intensity of a light?

2. What is the principle of photo electric transducer?

3. What is the Lambert’s Cosine Law?

4. What is the Inverse square Law?

5. Give three type of photo transducer?

a.

b.

c.

39

MESB 333 Lab No.4

Photo Transducer

1 Introduction.

In this lab, the students are to be expose to several type of photo transducer with their

characteristic that are related to Inverse Square Law and Lambert’s Cosine Law.

1.1 Objective

To understand the photo transducers effect and its relations with Inverse Square Law and

Lambert’s Cosine Law. Students will measure the effect of the incident light on the behavior of

a photodiode, phototransistor and photo conductive cell.

1.2 Theory

When light falls onto certain material, its energy will be given up as being described by the

principle of photo-electric transducer. The energy will become energy in the form of electric

current. Human eyes is an example of a photo-electric transducer. Eyes act as a transducer by

converting light energy to signals that will be sent to the brain for further process.

Experimentally, one can know the intensity of the light falls on an object by measuring the

corresponding electric current caused by the light. In this experiment, you will learn to use photo-

electric transducer to measure the intensity of light in relation to the induced current and

resistance.

The variety of colors existing in this world is due to the fact that sun-light has different

components of light. Color of light is determined by its frequency, which in turn proportional to

the reciprocal of its wavelength. The relationship between light frequency, speed of light and

wavelength is given in the equation

Where, f = frequency

v = speed of light, 3 x 108 m/s

= wavelength

= time to complete a cycle of wave

The spectrum for light with its wavelength has been measured experimentally as shown below.

1f

f

v

40

Table 4.1Spectrum for light

COLOR WAVELENGTH (mm)

Violet 440

Blue 470

Blue-Green 490

Green 520

Yellow-Green 550

Yellow 580

Orange 600

Red 690

Deep-Red 700

Light is a form of electromagnetic radiation. Alternatively, light can be considered as consisting

of little packets of energy, called photons, and the energy of each photon is directly proportional

to the frequency of light. From the light wavelength and frequency relationship, the smaller the

wavelength, the higher will be the frequency. With the relationship that energy is directly

proportional to the frequency of light, higher frequency will translate to higher energy. Therefore,

blue light has a higher energy that red light because the wavelength for blue light is shorter than

the red light as shown in table 5.1.

Luminous intensity for light has unit of candela, cd. 1 cd equals to 1/60 of luminous intensity

coming from an area of 1 cm2 of platinum melting at 2046 K. Light can be described in term of

luminous flux with a unit called LUMEN. A lumen is a luminous flux from a point source of 1

candela within a solid angle of 1 steradian. Luminous flux can be thought of as light power, or the

energy (number of photons) emitted per second.

Another definition is illumination. An illumination at any point on the surface is defined as

the luminous flux per unit area falling perpendicular to the surface. When a luminous flux of 1

lumen falls onto a surface area of 1 m2 , it is called an illumination of 1 LUX (lx)

1.3 The Inverse Square Law

If the radius of an imaginary sphere is increased from 1 m to 2 m, the area subtended

on the surface by the solid angle of 1 Sr is increased from 1 m2 to 4 m2, in proportion to the square

of the radius. The luminous flux over this area is still 1 m2 but the illumination has now fallen to

a quarter of its previous value as the luminous flux is spread over four times the area.

vf

f

v

2dE

41

Hence, the illumination on a surface is inversely proportional to the square of its distance from

the source. The illuminance, E (lux) is given as,

Where = luminous flux (lumen)

d = distance (m)

1.4 Lambert’s Cosine Law

If there is an angle of between the surface of the transducer and the oncoming light, the

luminous flux falling on the transducer surface is exactly the same as that which would fall on a

normal surface (Figure 5.1). However,

Area surface 1 = cos = Illumination surface 1

Area surface 2 Illumination surface 2

Figure 4.1

Thus the modification of the inverse square law becomes:

1.5 The Photo-Conductive Cell

A semiconductor, as its name implies is a material with an electrical conductivity in

between that of an insulator conductor and a conductor. Typical materials of interest are

Germanium and Silicon, but other materials and combinations of materials behave in a similar

fashion. They are extensively used in semiconductor devices, e.g diodes and transistors.

Electrical conduction in such a material occurs when free charge carriers, e.g electrons,

are available in the material to move when an electric field is applied. It happens that in certain

semiconductors, light energy falling on them is of the correct order of magnitude to release charge

carriers which will increase the flow of current produced by an applied voltage. This is known as

the PHOTO-CONDUCTIVE effect, and device is called a PHOTO-RESISTOR or a PHOTO-

CONDUCTOR, or sometimes a LIGHT DEPENDENT RESISTOR, as incident light will

effectively vary its resistance.

The current, or the number of charge carriers would expect to be related to the number of

1 2 Incident

Light

cosd

E2

42

photons, or the intensity of the incident light, and will be investigated. The colour of the light

will affect the response, due to the different energies of the photons. Small number of charge

carriers are also produced at room temperature by thermal effects, and this will also contribute to

the current.

The physical effects which cause this phenomenon are rather involved, but are given here to

make the study complete. In an intrinsic (pure) semi-conductor crystal all the valence electrons

have covalent bonds together with their neighbours. There may be represented on a diagram of

energy bands. It is found that there is a forbidden energy gap of the order of an electron volt

(1eV) between the valence band (where the electrons are bound to their parent atoms) and the

conduction band the electrons are now free charge carriers). This corresponds to the minimum

energy necessary to break a covalent bond and form a hole/electron pair. The electron is raised

into the conduction band and contributes to conduction as well as the hole left in the valence

band. This theory is fully described most standard textbooks. It is of interest to us now if this

energy can be supplied by light photons.

Consider first the effect of impurities in the semiconductor. Very small amounts of the correct

impurities can introduce either extra holes (P type) or extra electrons (N type) because atomic

structure. These will appear on our energy diagram as energy levels just below the conduction

band (doNor Ievel for N type) or just above the valence band (accePtor level for P type). If

photons of the correct energy illuminate such a specimen, several things may happen, as shown

in Fig 4.2

Figure 4.2 Effect of photons in energy bands of a semiconductor with both P & N type impurities

An electron/'hole pair may be generated by a high energy photon as described above. The

electron ‘jumps’ the gap into the conduction band. This is called intrinsic excitation.

An electron in the doNor level" (for N type) may be excited into the conduction band.

A valence electron may fill a hole in the accePtor level (for P type).

These last two transitions are known as impurity excitations and require less energy than

intrinsic excitations. However, the density of states in the conduction and valence bands greatly

exceeds the density of impurity states. At room temperature, most of the impurity atoms are

photon Impurity

excitation Intrinsic

excitation

Conduction band

doNor

level

AccePtor

level

Energy gap

Eg

Valence band

43

ionised in any case. Thus, photoconductivity is due principally to intrinsic excitation. Impurities

however do have advantages as discussed later. Our transducer is actually an N-type semi-

conductor.

The carriers generated by the photo-excitation will move if an external voltage is applied to

the device. This superimposes a regular drift on their random diffusion motion colliding with

others. They may however, recombine with an available hole or electron before they reach the

edges of the material. This may affect the response time of the device, cut down the available

current (loss of sensitivity) or introduce non-linearities. Those carriers remaining will constitute

the device current which thus depends initially on the number of photons.

The actual process is extremely complicated and depends on several factors, including the

density of the states in the energy bands, the probability that a photon will excite an electron, and

other factors, including carrier lifetime and mobility which depends upon recombinations and

trappings. Thermal effects also play a part.

1.6 SAFETY & PRECAUTION

1. Only plug the banana plug into the banana socket according to the experiment manual when

doing experiment, plugging the plug into the wrong socket may damage the electronics

component inside the control box.

2. Check the wiring connection between banana socket first before turn on the control box.

3. Do not connect the positive terminal of the power supply to negative terminal of the power

supply without connecting to any load between them.

4. Make sure the connection between the measurement point and the measurement meter are in

correct polarity.

5. Make sure the connection of the lamp to the power source are in correct polarity.

6. If the experiment is conducted during day light, take the reading as soon as possible in case

the day light varies. Also keep your hand away from the rig when taking readings in case they

cause unwanted reflections of light onto the transducers.

7. While the lamp is turn on, avoid touching the lamp’s body.

8. Before using the multi-meter to do voltage/current measurement, make sure the correct

measurement range is selected on the multi-meter. Also make sure the banana plug is

connected to correct terminal of the multi-meter.

Pre-experiment procedure

1. Read the safety instruction given before conducting the experiment.

2. Read and understand the theory of photo transducer before lab session.

3. Read and understand the theory of Inverse Square Law and Lambert’s Cosine Law before lab

session.

4. Prepare the accessories needed for the experiment.

44

2 Experiment 1: Photodiode

2.1. PROCEDURES

Part 1: Photo diode - Inverse Square Law

1. Make sure the control box’s main switch is turn off first before start doing wiring

connection.

2. Unplug all the banana plug from the banana terminal first before assembling out the circuit.

3. Start connecting the circuit using banana plug to respective banana socket, by using circuit

diagram below as reference.

4. Make sure all the wiring connection is according to the circuit diagram. Before switch on

the power supply, let the lab instructor to check the connection of circuit.

5. Plug in the lamp’s banana plug into the Lamp’s power supply banana socket, make sure the

polarity is correct.

6. Adjust the position of the photo transducer box so that its angular scale of the photodiode

facing the light source is 0°.

7. Ensure the hole of the photo transducer box is not facing other light source, affecting your

reading value during experiment.

8. Turn on the mains switch, wait all the measurement meter initialized first before start

conducting experiment.

9. Switch on the lamp’s power supply, check whether the lamp got light up or not.

10. Adjust the position of the light facing the photo transducer box, while carefully adjusting

the position of the lamp with distance 1 meter.

11. Move the bulb to get different distance.

12. At each value of different distance, record down the values of the voltage and current on

your table.

Part 2: Photo diode - Lambert’s Cosine Law

1. With the circuit of Part 1 still connected, return the photo transducer box and lamp to their

starting positions (distance 1 meter)

2. Switch on the lamp again.

3. Rotate the angular scale shown on the photo transducer box to 30° anti-clockwise and

record the reading.

4. Repeat the procedure 3 for the angles as shown in the table below.

Fig. 4.3 - Schematic for the photodiode experiment

45

5. After finish the experiment, switch off the lamp power supply and the main power supply

switch on the control box.

2.2. RESULT AND DISCUSSION

Part 1: Photo diode - Inverse Square Law

Table 4.2 Experiment Result of Photo diode response

Applied voltage:_____________Volt

Distance (m) Current (μA) Resistance (Ω)

1000

900

800

700

600

500

400

300

200

100

Switch Off the

lamp

For each distance, calculate the resistance of the transducer by applying Ohm’s law and

dividing the applied voltage by the current flowing, R = Vdc/I

What is the relationship between resistance and distance at constant voltage?

Why the current did not become zero when the lamp is switch off?

How can you relate the result obtained with Inverse Square Law? Plot graph if required?

Plot a graph of current flowing against distance. Label your graph with the value of applied

voltage. Discuss the shape of the graph.

46

Part 2: Photo diode - Lambert’s Cosine Law

Table 4.3 Experiment Result of Photo diode - Lambert’s Cosine Law

Angle (Degrees) Current (μA) Resistance (Ω)

30 (ACW)

25

20

15

10

5(CCW)

0

5 (CW)

10

15

20

25

30

Plot a graph of current flowing against angle.

Does the graph follow accurately the cosine law?

Suggest the principal advantages and disadvantages of the Photo diode.

47

3 Experiment 2: Photo Conductive Cell

3.1 Procedure

Part 1: Photo Conductive Cell - Inverse Square Law

1. Make sure the control box’s main switch is turn off first before start doing wiring

connection.

2. Unplug all the banana plug from the banana terminal first before assembling out the circuit.

3. Start connecting the circuit using banana plug to respective banana socket, by using circuit

diagram below as reference:

4. Make sure all the wiring connection is according to the circuit diagram. Before switch on

the power supply, let the lab instructor to check the connection of circuit.

5. Check the potentiometer (VR) control knob on the Operational Amplifier section of the

control box is set to minimum first.

6. Plug in the lamp’s banana plug into the Lamp’s power supply banana socket, make sure the

polarity is correct.

7. Adjust the position of the photo transducer box so that its angular scale of the photodiode

facing the light source is 0°.

8. Ensure the hole of the photo transducer box is not facing other light source, affecting your

reading value during experiment.

9. Adjust the multi-meter’s rotary switch into the correct range. i.e. 200mA range for current

meter and 20V for voltage meter.

10. Turn on the mains switch, wait all the measurement meter initialized first before start

conducting experiment.

11. Switch on the lamp’s power supply, check whether the lamp got light up or not. After that,

position the lamp holder again at the distance of 1meter.

12. Adjust the potentiometer to get 10mA. Record down the voltage and this value should be

constant for the experiment.

13. Leave the equipment like this for at least 5 minutes. This is to ensure the necessary pre-

conditioning of the device is carried out.

14. Move the lamp backwards to vary the distance and the affect on the transducer. Record the

voltage and current value at each step.

15. Switch off the lamp and take the reading again corresponding to ambient light illumination.

Part 2: Photo Conductive Cell : Lambert’s Cosine Law

Fig. 4.4 - Wiring Diagram for Photo Conductive Cell Experiment

48

1. With the circuit of Part 1 still connected, return the photo transducer box and lamp to their

starting positions.

2. Switch on the lamp again and slowly adjust the potentiometer (VR) until the multi-meter

reads about 10mA initial value.

3. Rotate the angular scale shown on the photo transducer box to 30° anti-clockwise and

record the reading.

4. Repeat the procedure 3 for the angles as shown in table below.

5. After finish the experiment, switch off the lamp power supply and the main power supply

switch on the control box.

3.2 RESULT AND DISCUSSION

Part 1: Photo Conductive Cell- Inverse Square Law

Table 4.4 Experiment Result of Photo Conductive Cell response

- Plot, discussion, analysis and conclusion.

Distance (mm) Current (mA) Voltage

(Volt)

Device Resistance

(Ω)

1000

900

800

700

600

500

400

300

200

100

Off of the lamp

49

Part 2: Photo Conductive Cell - Lambert’s Cosine Law

Table 4.5 Experiment Result of Photo Conductive Cell Lambert’s Cosine Law

Angle (Degrees) Current (μA) Resistance (Ω)

30 (ACW)

25

20

15

10

5

0

5

10

15

20

25

30

- Plot, discussion, analysis and conclusion.

50

4 Experiment 3: Phototransistor

4.1 Procedure

Part 1: Phototransistor - Inverse Square Law

1. Make sure the control box’s main switch is turn off first before start doing wiring

connection.

2. Unplug all the banana plug from the banana terminal first before assembling out the

circuit.

3. Start connecting the circuit using banana plug to respective banana socket, by using

circuit diagram below as reference:

4. Make sure all the wiring connection is according to the circuit diagram. Before switch on

the power supply, let the lab instructor to check the connection of circuit. 5. Check the potentiometer (VR) control knob on the Operational Amplifier section of the

control box is set to minimum first.

6. Plug in the lamp’s banana plug into the Lamp’s power supply banana socket, make sure

the polarity is correct.

7. Adjust the position of the photo transducer box so that its angular scale of the photodiode

facing the light source is 0°.

8. Ensure the hole of the photo transducer box is not facing other light source, affecting your

reading value during experiment.

9. Adjust the multi-meter’s rotary switch into the correct range. i.e. 200mA range for

current meter and 20V for voltage meter.

10. Turn on the mains switch, wait all the measurement meter initialized first before start

conducting experiment.

11. Switch on the lamp’s power supply, check whether the lamp got light up or not. After that,

position the lamp holder again at the distance 1 meter.

12. Adjust the potentiometer to get different voltage.

13. Leave the equipment like this for at least 5 minutes. This is to ensure the necessary pre-

conditioning of the device is carried out.

14. Move the lamp backwards to vary the distance and affect on the transducer. Record the

voltage and current value at each step.

15. Switch off the lamp and take the reading again corresponding to ambient light

illumination.

Fig. 4.5 - Wiring Diagram for Photo-transistor Experiment

51

Part 2 Phototransistor - Lambert’s Cosine Law:

1. With the circuit of Part 1 still connected, return the photo transducer box and lamp to

their starting positions corresponding to 100% relative illumination.

2. Switch on the lamp again and slowly adjust the potentiometer (VR) until the multimeter

reads about 10mA initial value.

3. Rotate the angular scale shown on the photo transducer box to 30° anti-clockwise and

record the reading.

4. Repeat the procedure 3 for the angle of 20°, 10° until 0° up to 30° clockwise.

5. After finish the experiment, switch off the lamp power supply and the main power supply

switch on the control box.

4.2 RESULT AND DISCUSSION

Part 1: Phototransistor - Inverse Square Law

Table 4.6 Experiment Result of Phototransistor - current Response

Distance (mm)

1000 900 800 700 600 500 400 300 200 100

Voltage

(V)

Current (mA)

0

1

2

5

10

- Plot, discussion, analysis and conclusion.

52

Part 2: Phototransistor - Lambert’s Cosine Law

Table 4.7 Experiment Result of Phototransistor - Lambert’s Cosine Law

Angle (Degrees) Current (μA) Resistance (Ω)

30

25

20

15

10

5(CCW)

0

5(CW)

10

15

20

25

30

Plot graph and write the analysis according to the objective of the experiment.

53

MESB 333 LAB NO. 5 :

FLOW RATE MEASUREMENT

PRELAB QUESTIONS

Name: _____________________SID: ______________ Group:______ Date:_______________

1. What are the examples of flow measurement techniques that use obstruction.

2. Draw the cross section of a venturi meter and label the throat, upstream, and recovery cone.

3. Why is orifice plate is used as a fluid flow measurement device?

_________________________________________________________________________

4. What is discharge coefficient ? What are Cd for orifice plate and venturi meter ? What

does the Cd value tells us ?

________________________________________________________________________

________________________________________________________________________

5. What does smaller discharge coefficient tells us?

54

MESB 333 Lab No. 5

Flow Rate Measurement

1 Objective

In this experiment, students will learn different types of flow meters devices to measure liquid (water) volume flow rate. The flow meters used on the apparatus are venturi meter, variable area meter and orifice plate. From these three devices, you will be able to compare the advantages and accuracy of each device.

1.1 Theory

The theory behind this experiment is similar to the air flow rig in experiment 2. From the pressure drop on the orifice or the venturi meter, the flowrate of the fluid can be calculated.

Applying Bernoulli equation:

For same elevation, Z1 = Z2 Carry the velocity to the right and pressure to the left:

Now, we will write the above in term of V2:

22

22

11

21 Z

g

P

g2

VZ

g

P

g2

V

g

P

g2

V

g

P

g2

V 2221

21

21

2221

21

2221

VVg2

1PP

g

1

g2

V

g2

V

g

P

g

P

:gives)VV(g2

1)pp(

g

1ointVSubstitute

VA

AV

VAVAQ

:flowidealanFor

21

22211

21

21

2211

2

1

222

21

22

2

1

22221

A

A1

2

Vpp

VA

AV

g2

1)pp(

g

1

2

1

2

212

2

1

2

2122

A

A1

)pp(2V

A

A1

)pp(2V

55

Knowing that Qideal = A2V2, thus:

The above is for an ideal flow. For venturi tube and the orifice, the equation must be

multiplied with the coefficient of discharge, Cd:

Where,

Cd : discharge coefficient Q : volume flowrate (m3/s) A2 : throat diameter for venturi, or orifice diameter for orifice plate A1 : upstream pipe diameter

P : (P1-P2) pressure drop across the venturi meter or the orifice (gh) Cd values assumed to be: Cd = 0.98 for the venturi meter Cd = 0.63 for the orifice plate

1.2 Discharge Coefficient

What is really a discharge coefficient? You have observed in the previous experiments on the airflow rig where the discharge coefficient is always used in relation to the orifice plate and the nozzle. Similarly, discharge coefficient will be applied to venturi tube too. Discharge coefficient basically tells how much the actual flow defers from the ideal flow:

A smaller value of discharge coefficient tells that the actual flow is smaller compare

to the ideal or theoretical value. The discharge coefficient for the orifice plate is 0.63

while for the venturi meter it is 0.98. There is more resistance to the flow imposed by the

orifice plate, and subsequently it causes some loses through the meter. This loss can be

observed from the large pressure drop across the orifice compares to the pressure drop

across the venturi meter.

ideal

actuald

Q

QC

2

1

2

212ideal

A

A1

)pp(2AQ

2

1

2

212dactual

idealdactual

A

A1

)pp(2ACQ

QCQ

56

1.3 Apparatus

Figure 1

Experiment

apparatus

The hydraulic bench and the apparatus are as shown above. The flow meter apparatus

is set up on top of the hydraulic bench. The apparatus above consists of venturi meter,

variable area meter and orifice plate and 8 bank manometer. Pressure readings of the

water flow will be taken from the 8 bank manometer.

1.3.1 Technical Data:

Venturi meter Upstream pipe diameter = 31.75 mm hence A1 = 7.92 x 10-4 m2 Throat dia. = 15 mm hence A2 = 1.77 x 10-4 m2 Upstream taper = 21 0 inclusive Downstream taper = 14 0 inclusive

Orifice plate

Upstream pipe diameter = 31.75 mm hence A1 = 7.92 x 10-4 m2

Orifice diameter = 20 mm

hence A2 = 3.14 x 10-4 m2

1.4 Procedure

1. Observe that the apparatus is placed on the hydraulic bench. The inlet pipe of the apparatus is connected to the hydraulic bench supply, while the apparatus outlet pipe is connected to the pipe going to the volumeter tank.

2. Note that the hydraulic bench inlet valve is in shut position. 3. Switch on the pump then slowly open the hydraulic bench inlet valve. 4. At the same time open the flow control valve, the outlet valve on the apparatus. 5. To disperse air trapped in the flow system, close flow control valve, open air bleed screw and

57

prime manometer and tappings. When done, close back the air bleed screw. 6. Switch off the pump and adjust the levels of the manometer by adjusting the air bleed screw.

Try to get initial manometer level at a comfortable level so that when experiment is carried out there will be enough room for the water column in the manometer to move up and down. Close back the air bleed screw when done. Switch on the pump again.

7. Adjust the inlet and outlet valves so that variable meter gives the flow rate of 2 Liter/min. Record the manometer reading. Increase the flow rate until 22 Liter/min.

8. Measure a certain volume of the reservoir, using stop watch measure the time taken to fill that portion.

9. Repeat step 7 to get another set of data.

1.5 Results

Get the manometer readings for the respective flow rates of the variable meter. Table 1 Experiment Result

Variable Meter

Flow rate (Liter/min)

Manometer Readings (mm)

1 2 3 4 5 6 7 8 Seconds

2

5

10

12

15

18

20

22

Note the followings: Manometer 1 minus Manometer 2 = Venturi Reading Manometer 1 minus Manometer 3 = Loss In Venturi Manometer 4 minus Manometer 5 = Loss In Variable Area Manometer 6 minus Manometer 7 = Orifice Plate Reading Manometer 6 minus Manometer 8 = Loss In Orifice Plate

From the readings obtained on the Venturi meter and orifice plate calculate the volume flow rate using the basic equation with relevant Cd factor.

Note that (p1 - p2) in the equation refers to Venturi Reading (Manometer 1 minus Manometer 2), and NOT Loss In Venturi (Manometer 1 minus Manometer 3). Similarly for Orifice Plate, use Orifice Plate Reading.

Calculate the actual flow rate using the volume and time measured.

Don't forget to change the manometer column readings from mm to m.

Compare these calculated values and the reading on the variable area meter with the actual flow rate. Use same units.

Calculate the velocity at point 2 (venturi meter) and 7 (orifice plate) (Use formula: velocity=volume flow rate/cross section area) and discuss.

Also calculate the Reynolds number at these two points. Red = Dv/,,where = absolute viscosity = 8.937 x l0-4 Pa.s and D is the diameter of the holes.

Question for discussion

When calculating (p1 - p2) for the venturi meter, why is the reading for p2 is taken at the venturi throat and not at the tapping after the throat?

How does the variable area meter work? How to calculate the volume flow rate using stop watch?

What sort of losses do you think occur on the venturi meter and the orifice plate?

Why the heights should different in relation to the others in the manometer?

Why velocity at P2 and P7 are different?

58

Which flow meters devices as the smallest error? Include error analysis.

Flowrate comparision table Variable Meter

Flow rate (Liter/min)

Conversion to

m3/s

Venturi Flowrate

m3/s

Oriface Flowrate

m3/s

Flowrate using

stopwatch m3/s

2 5

10 12 15 18 20 22

Percentage Different Relative to Variable Meter Variable Meter

Flow rate (Liter/min)

Venturi %

Oriface %

Stopwatch %

2

5

10

12

15

18

20

22

Velocity at p2 and p7. Variable Meter

Flow rate (Liter/min)

Velocity at P2 m/s

Velocity at P7 m/s

Reynolds Number

at P2

Reynolds Number

at P7

2 5

10 12 15 18 20 22

Lab No.6

47

MESB 333 LAB NO. 6:

INTRODUCTION TO PID CONTROLLER

PRELAB QUESTIONS

Name: _____________________ SID: ______________ Group:______ Date:____________

1. What is the difference between a open-loop control and close-loop control?

2. Draw the three main test signals : step, ramp, sinusoidal

3. Describe what do you understand about the control actions: proportional, derivative and Integral.

4. Draw an example of a system response with depict peak overshoot, settling time, rise time and

steady state error.

5. What are the three types of response for a second order system?

Lab No.6

48

MESB 333 Lab No. 6

Introduction to PID Controller ______________________________________________________

1 Objective

Design the experiment in order:

1. To investigate and learn the importance of the vital system characteristics in the assessment

of control loop efficiency.

2. To evaluate the PID control elements using the PCU computer controlled flow cycle.

1.1 Theory

A. Introduction to Control System

In the industrial world the field of control engineering is very crucial. Control systems are

designed to achieve specified objectives within a given set of constraints. The three common

control strategies are open-loop, feed forward and closed-loop control. The open-loop control

cannot compensate for either disturbances to the system or changes in plant parameters (Figure

7.1). For example an open-loop speed control system cannot compensate for load variation

(disturbance) and the bearings friction variation (plant parameter).

Figure 6.1 Open Loop Strategy

The feedforward control attempts to compensate for disturbances before they have any effect

on the system output (Figure 6.2). This strategy can be effective if the disturbance can be

measured. However it cannot compensate for changes of the plant parameters which cannot be

measured and treated as a disturbance.

Figure 6.2 The Feed Forward Strategy

The most common control strategy is feedback or closed loop control, as illustrated in figure

6.3. Here the process output is monitored, and control actions are taken to counteract deviations

Input

(desired behavior)

Controller Control

Action

Process

s

Output

(actual behavior)

Input

(desired behavior)

Controller Control

Action

Process Output

(actual behavior)

Disturbances

Measure Disturbances

Lab No.6

49

from the required behavior. In the case of motor speed control system, the speed is measured,

and the applied voltage is modified as required. However in practice, feedback and feedforward

are often combined in a single system.

Figure 6.3 the Closed-loop (feedback) Control Strategy

B. PID Controller

The term PID controller refers to proportional, integral and derivative controller. PID

controllers are the most common controller used in the industrial process control.

I) Proportional Control Mode

In this mode the output of the controller is proportional to the error between the set point

and the measured value. Proportional control may be expressed as either proportional gain

or proportional band. Mathematically ,

Mp =PG(SP-MV)+C = PG e(t) +C

Where, Mp = Controller Output

PG = Proportional Gain

SP = Set point

MV = measured value

C = Output with zero error

e(t) = Error as a function of time.

The error band where the output is between 0% and 100% is called the proportional band

(PB), and given by PB = 100/PG. Thus the higher the gain the smaller the band. This control

mode rarely produce adequate control, where there usually an offset (permanent error).

II) Integral Mode

This mode of control is often used to remove proportional offsets errors. The integral mode

determines an output based on the history of error. It is calculated by finding the net area under

the error curve versus time and multiplying by a constant called the integral action time (IAT)

in seconds. The controller output equation is:

The integral Action time is defined as the time taken for the integral action to duplicate the

Input

(desired behavior) Controller

Control

Action

Process Output

(actual behavior)

Disturbances

Measure

dt)t(eIAT

PG)t(Mi

Lab No.6

50

proportional action of the controller, if the error remains constant during this period. It is used

commonly to remove any steady state errors incurred when using a proportional controller.

III) Derivative Control Mode

Derivative control mode is often used to reduce the response time of the system, it is based

on the time rate of the change of error. The time taken for the proportional action to duplicate

the instantaneous output of the derivative element is called derivative action time (DAT). The

controller output equation is:

The derivative control mode is never used alone as there is no controller output

corresponding to zero rate of change. So it is commonly used with Proportional controller

(PD). However, it can also exaggerate high frequency noise in the system.

C. System Response

Figure 6.4 shows the typical system response of a control system. There are three types of

response for a second order system, which are overdamped, underdamped, and critical

damped response. The system response depends on the PID gains set in the experiment. The

characteristics of the response is shown in Figure 6.5.

Figure 6.4

dt

)t(deDATPGMd

Lab No.6

51

Figure 6.5

Some of the important system performance parameters are:

Peak overshoot : is often expressed as percent overshoot at the first peak and given by (Peak

value- input value)/input value * 100

Settling time: The time taken to settle within 2% of the final value

Rise time: The time taken for the system to respond to a fraction of the final value on the initial

part. Typically 5-95% or 10-90%.

Steady state error: Any error between the set point and the controlled variable once the system

has stabilized.

1.2 Apparatus

1.2.1 The System Rig

The System Rig is the hardware for the process, which is to be controlled by the

microcomputer. This reflects a typical process control situation such as in the food and drink

manufacturing petrochemical industry.

Each feature on the System Rig has a manual or computer control option. Users may select

either of the modes allowing a comparison between human and computer control operation to be

made. This allows a rapid appreciation of the advantages and disadvantages under both modes of

control.

Lab No.6

52

1.2.2 Description

Figure 6.6 Process control unit

LEGEND

A - Mains switch G - Overflow pipe

B - Water pump switch H - Proportional valve

C - Bottom reservoir tank I - Water inlet port

D - Bypass valve J - Water drain port

E - Return valve K - Water pump

F - Water level tank L - Control panel

M - Level foot

Lab No.6

53

SAFETY / PRECAUTION

1. Ensure that there are sufficient water in the bottom reservoir tank before conducting the

experiments.

2. Make sure there are no leakages in the piping system before conducting the experiments.

3. Open the bypass valve before switching on the water pump and close it only after the flow is fully

circulated through the entire system for a brief period.

MANUAL SETUP

1. Place the LS-33039 PID Controller Experiment Rig. On a level table and adjust the levelling foot

if necessary.

2. Connect the main power plug to electrical supply.

3. Connect the RS-485 cable from the computer to the control box.

4. Run the Data Acquisition Software from the computer

5. Switch on the mains switch on the control box

6. Ensure there is enough water in the bottom reservoir tank before switching on the pump.

7. The LS-33039 apparatus is ready to be used.

MAINTENANCE

1. Please check for signs of leakage in the piping system from time to time. Besides that there is no

major maintenance required for this apparatus

2. Kindly seek the assistance from the manufacturer if necessary.

1.2.3 Feedback

Feedback is an essential requirement for the control of any process. It consists of various

transducers measuring the conditions on the rig and feeding this information back to the

controlling microcomputer.

On the Process Control Unit the temperature at the sump, flowline and process tank are

measured using platinum resistance thermometers. The flowrate is measured by an in-line

flowmeter. These analogue signals are fed back to the signal conditioners on the Computer

Control Module (CCM) from where they are sampled by the microcomputer via an analogue to

digital converter (ADC). LED meters are used to display the temperatures and flowrate on the

system rig. Indicators are provided for the cooler, tank full sensor and drain/divener solenoids,

giving a status check when the Process Control Unit is in operation.

1.2.4 Flow measurement

The flow rate of the fluid is measured by means of a flow meter of the impeller type. The fluid

flows through the meter rotating the impeller, which has six blades. Mounted either side of the

impeller is an infra red transmitter and receiver producing an infra red beam which is broken by

the rotating impeller. Six pulses are therefore produced for one revolution of the rotor, thus

producing a frequency output 'which is proportional to the flowrate.

Lab No.6

54

The approximate full-scale frequency is 570Hz (pulses/sec) which is converted to a voltage

by the signal conditioning circuit. This voltage is used to drive the flowrate LED display on the

rig and also converted into a digital word by the Data Acquisition circuit.

Figure 6.8

1.2.5 Pump

The pump used is a centrifugal type. It is not a positive displacement type and thus its output

is not necessarily linearly proportional to speed, though variation in speed will, of course, vary

the output flow rate.

Activating Voltage: 12V D.C; Maximum Continuous Current: 6 Amps

1.2.6 Water Drain Port

This is used to drain the bottom reservoir tank

1.3 Software Operation

a) Turn on both the computer system and the process control unit.

b) In the Windows desktop, select the LS-330390 PID icon.

c) In the program, follow the instructions in section 1 to familiarize yourself with the program.

1.3.1 Section 1: Assessment of System Performance

1. By operating the controls in the Process Control Unit, the vital characteristics can be easily

demonstrated by varying the values of the PID controller.

2. Select the Flow Control tab and in the Control select the Closed Loop tab

3. Set the “Set point” to 4 liter/min and set the controller setting as in the table below.

4. Click the Enabled button to start the flow.

5. Set the PID controller using the given values. Use your own values to complete the table.

6. Print out your results and observe the graphs. Label the graphs.

7. To study the effect of load change on the PID controller. Based on the plotted response from

Table 1, select the best PID controller response, introduce a disturbance by opening the by-

pass valve 30% when it has reached the stabile flow rate. Observe the response of the

controller and comment on the behavior.

Lab No.6

55

1.3.2 Section 2: Evaluation of the PID Control Elements

The PID control elements may be easily evaluated using the PCU computer controlled flow cycle.

Characteristic selection of PID elements:

The selection range of the PID elements is:

Proportional Gain: Between 1 to 10

Integral Action: Between 0 to 1

Derivative Action: Between 0 to 1

Base on Software operation in 1.3, construct the experiment procedure in order to achieve

the objective.

Lab No.6

56

MESB 333 Lab No. 7

Free and Damped Vibration ______________________________________________________

Introduction

In this lab, the students are to be expose to several type of free and damped vibration system with

their characteristic that are related to the theory learn in class.

1.1 Theory

Underdamped Syatem

The displacement solution for this kind of system is:

An alternate but equivalent solution is given by:

The displacement plot of an underdamped system would appear as:

Note that the displacement amplitude decays exponentially (i.e the natural logarithm of the amplitude ratio

for any two diaplacements seperated in time by a constant ratio is a constant)

Lab No.6

57

, Td is the period of the damped vibration.

Critically Damped System

The displacement solution for this system is:

The critical damping, Cc can be interpreted as the minimum damping that results in non-periodic

motion (i.e sample decay). The displacement plot of a critically-damped system with positive initial

displacement and velocity would appear as,

The displacement decay to a negligible level after one natural period, Tn. Note that if the initial

velocity V0 is negative while the initial displacement X0 is positive, there will exist one overshoot of

the resting position in the displacement plot.

Overdamped System

The displacement solution for this kind of system is:

The displacement plot of an overdamped system would appear as:

Lab No.6

58

The motion of an overdamped system is non-periodic, regardless of the initial conditions. The larger the damping, the longer the time to decay from an initial disturbance.

If the system is heavily damped, ζ > 1, the displacement solution takes the approximate form:

EXPERIMENT I

1 Objective

To determine the spring coefficient and to investigate the deflection of the spring at certain

load.

1.2 Procedure

1.3 Result and Discussion

1. Find out the spring constant, k for spring T1, T2, T3.

2. Plot a graph of force against deflection, where the spring coeffiecient is the slope,

m of the graph. The k value is in unit kg/mm or N/mm.

Lab No.6

59

EXPERIMENT II

1.1 Objective

To determine the spring coefficient and the natural frequency of single degree freedom.

1.2 Procedure

1.3 Calculation:

Use the formula below to calculate the natural frequency.

where,

k=stiffness (N/m)

m=mass (kg)

RPM of the motorized chart recorder = 5 rpm

Diameter of drum collector = 27.00mm and the circumference=84.82

𝒇𝒏 =𝟏

𝑻

Where,

T:time (seconds)taken to complete one cycle.

Lab No.6

60

1.4 Result and Discussion:

1. Compare natural frequency of the system between the calculated from plotted graph and formula.

2. Find out the spring constant, k from Experiment 1.

3. Repeat the experiment and observe the behaviour of different type of spring.

EXPERIMENT III

1.1 Objective

1. To demonstrate the oscillation of single degree freedom system

2. To investigate the behaviors for free vibration and damped vibration

1.2 Procedure

1.3 Calculation:

Calculate the natural frequency of the system as experiment 2.

,

The damping ratio can be obtained from the formula above

1.3 Result and Discussion:

Lab No.6

61

Do discuss if the damper is underdamped, critically damped or overdamped system.

**Please do download the details manual from the Moodle. **