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Department of Mechanical Engineering Strength of Materials
1
Strength of Materials
Mr. Sunil Pandey
Department
of Mechanical Engineering
ECHELON INSTITUTE OF TECHNOLOGY
NAME ------------------------------------------------------------------- ROLL NO.--------------------------------------------------------------- BRANCH---------------------------------------------------------------- BATCH-------------------------------------------------------------------
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Content
S.No. Content Page No.
General Instructions 3
1. To perform the tensile test on UTM 8
2. To perform the compression test on UTM 19
3. To perform the bending test on UTM 24
4. To perform the shearing test on UTM 29
5. To perform the tensional test on Torsion testing machine 33
6. To perform hardness test on hardness test machine 40
7. to perform toughness test on toughness test machine. 49
8. To perform fatigue test on fatigue test machine. 56
9. To perform cupping test on cupping test machine. 60
10. To study the behavior of column with various end
conditions.
71
11. To verify the moment area theorem regarding the slopes and deflections of the beam
77
12. To determine the elastic properties of beam. 77
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General Instructions
To make laboratory experiments safe and effective, each student should follow the given
instructions.
SAFETY
1. High voltage source in the laboratory should be handled properly under the
guidance of lab assistant, as it may cause a serious accident.
2. Avoid loose clothes, shirts should be properly tucked, skirts with extra flares
should be avoided, slippers are not allowed, shoes with rubber soles are
recommended for mechanical work laboratories.
3. Make sure that all power sources are off during set-up of machines.
4. Keep safe distance from moving parts of machines.
5. Follow the instruction given by the instructor
6. Failure to obey instructions may result in being expelled from the lab
7. Be careful not to damage any machine or instrument. Care must be taken in
handling all instrument
8. Do not start any machine or operate it without the permission from instructor.
9. Lubrication should be checked before starting the machine if required.
10. The application or removal of the load should be gradual.
11. Any unusual behavior or noise of the machine must be reported immediately
reported to the instructor and investigated
ATTENDANCE
1. All students are required to attend and contribute adequately while
performing experiments in the group.
2. The punctuality in attendance in the laboratory is essential. The student
should not leave the lab without permission
3. All students must write satisfactory report for each lab experiments.
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4. Failure to be present for an experiment will result in losing entire marks
for the corresponding lab.
5. All students are supposed to attend only their group of experiment
assigned at the beginning of the lab.
PREPARATION OF LAB REPORT
1. Before coming to the laboratory, each student must read and review
appropriate experiment to be conducted on the subsequent turn.
2. Record your experiment observations and sample calculations carefully.
3. Each student is required to write a neat and clean report for the experiment
conducted.
4. Every student should bring his own set of drawing instruments logbooks,
slide rule etc
5. Student should get the necessary apparatus issued against their names
before starting the experiment should carefully inspect the apparatus and
returned it well to the lab in charge after finishing the work
6. Reports are due one week after the completion of the experiment.
7. Each report shall be submitted with all necessary instructions, sample
calculations, graphs, and discussion over data and graph.
8. Observations should be recorded in tabular form and in a proper order
9. Sample calculations should be done on a set of most important data. The
calculations should be complete, leading from observed quantities to final
results
10. Results within the scope of the object should be given, with graphical
representation wherever possible.
11. Sources of error should be reported properly. It provides a limit for
admissible inaccuracy in the results.
12. Discussion over results should be analyzed properly and compared with
the manufactures rating.
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13. A brief criticism of the test procedure and apparatus used with concrete
suggestions, if any, for improvement should be explained. Any unusual
occurrence observed during the test should be reported.
1. Discussion should reflect the opinion of the writer. It should not be a
collection of merely the self-evident facts.
2. Questions give at the end of each experiment have to be answered
appropriately with in the space provided in the manual.
3. Students should remain prepare for the viva-voce on any turn.
HOW TO PLOT A GRAPH
1. Before drawing a graph between two observed variables it is necessary to
know the nature of expected theoretical graph.
2. Decide which parameter to be considered on X axis and which one on the
Y-axis.( parameter which is under the control of the student is generally
kept over X axis)
3. Selection of appropriate scales for the two variables should be chosen such
that it appears as square graph.
4. The following procedure should be observed in drawing the graphs.
(i) A curve should first be drawn freehand in pencil. It should then be
faired, preferably in black ink, with proper instruments.
(ii) Unless otherwise specified, the independent variables should be
plotted on the abscissa.
(iii) The axes should be well defined and bold.
(iv) The scales should be chosen for easy reading with due regard to the
accuracy of the observed quantities so that variations are neither
concealed nor exaggerated. Too large a scale should not be chosen
simply to fill a curve sheet. Some times the scale of abscissa may be
taken larger than ordinate to make the curves clear.
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(v) The scale for the axes may or may not start from zero; but scale for the
curves of efficiency, economy rate, capacity, etc should always start
from zero.
(vi) When several curve are drawn over the same abscissa, care must be
taken in choosing the ordinates of the scales such that the curves do
not overlap confusingly.
5. Different indent points should identify each curve separately.
6. Points plotted should be joined such that it appears smooth and near to the
theoretical nature of the curve. It is not necessary to join all points on the
graph. Average graph is always advisable, instead of point
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PREFACE
There was a long felt demand by faculty and students for a comprehensive lab manual on
Strength of Materials, studied in engineering branch affiliated to M.D. University Rohtak.
This increasing demand encouraged the authors to come up with an illustrative write up
of the experiments.
All necessary guidelines have been given in this manual although on the time basis each
and every necessary step will be told to students at the time of performing a particular
experiment.
Ten selected experiments have been presented in the well suitable manner and are
expected to be student friendly.
This manual looks for the betterment of students and will be amended on the time basis.
This manual aims the practical performed for the strength of material subject of echelon
institute of technology Faridabad. Teachers copy of the experimental results and answer
for the question are available in the lab as sample guidelines.
We hope that this manual would be a great help for students of Mechanical Engineering
branch . Any suggestion, constructive criticism for further improvement of manual will
be accepted wholeheartly.
Author express gratitude to Management of Echelon Institute of Technology, Faridabad
for their continuous encouragement for the successfully completion of this difficult task.
I also express very thankful to those people who, directly or indirectly was involved in
this task.
Author
Sunil Pandey
June, 2012
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Experiment No. 1 Name__________________RollNo._________Group/BatchNo.____________
Date ________Marks/Grade__________Facultys Signature______________
AIM: - To perform the tensile test on UTM EQUIPMENT REQUIRED: Tensile testing machine, steel rule, specimen
THEORY- When a specimen is axially pulled under static loading conditions, the specimen
elongates and finally breaks. The elongation per unit length is called strain and the load acting
per unit cross- sectional area is called stress. The corresponding stress is called proportional
limit and the slope of straight line is called modulus of elasticity. Up to a particular load the
specimen regains its original dimensions upon removal of load. Beyond that load some
permanent deformations remains. The corresponding stress is called elastic limit. The
elongation less than that corresponding to the elastic limit is called elastic deformation,
elongation greater than that corresponding to the elastic limit is called plastic deformation.
After a particular load, the material elongates even when the load is kept constant. Since the
strain rate is low, the load has to be decreased to effect the elongation. The stress
corresponding to initial load is called upper yield point and that corresponding to decreased
constant load is called lower yield point and the phenomenon of elongation at constant load
corresponding to lower yield point is called yielding. After a particular load the specimen
undergoes localized deformation leading to sudden decrease in cross-sectional area and large
increase in elongation . The specimen breaks. The material which are weak in shear fail along a
plane of 45 degree to the axis - where the shear stresses are maximum .The materials which are
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weak in tension fail along a plane 90 degree to the axis, where the tensile stresses are
maximum. The energy absorbed per unit volume during the elastic deformation is called
modulus of resilience and is given by E2
2 . The energy absorbed per unit volume up to
rupture is given by the area under the curve and is called modulus of toughness. Materials
with strain less than 5% at fracture are regarded as brittle and those having strain more than 5%
at fracture are regarded as ductile. For materials which do not show yielding, a tangent to the
curve is drawn at the origin and is offset by 0.2% strain. The stress corresponding to the point
of intersection of the offset tangent with the curve is called proof stress. The strain
corresponding to the UTS is called maximum uniform strain. The percentage of elongation,
percentage of reduction in area and maximum uniform strain is used for comparing ductility of
materials. The ratio of load to original Cross-sectional area is called engineering stress and
ratio of load to current area is called proof stress. Similarly true strain is defined as summation
of incremental strains over the- entire load range. Some materials show increase in yield
strength when loaded to plastic range, unloaded and then reloaded. This phenomenon is called
strain hardening.
REQUIREMENTS- An arrangement to hold a specimen and pull it axially at a uniform preset
rate. An arrangement to measure the load acting on the specimen. An arrangement to measure
the elongation of the specimen.
DESCRIPTION OF APPARATUS - Three load scales for indicating the load acting on the
specimen. Three counter weights for use in different combinations corresponding to each of the
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three load scales Each load scale is for different range of loads and selection of any particular
scale for an experiment depends on the expected load range for the particular specimen used in
the experiment. A linear displacement measuring scale for indicating the elongation of the
specimen. A motor gear- box assembly with belt and pulley arrangement for obtaining
different speeds. A screw attached to the motor foundation for loosening and tightening the
belts so that the desired pulley combination is achieved. A vertical bolt is connected to the
gearbox output shaft. A nut on the vertical bolt. A cross slide welded to the nut at the center
and which slides on two vertical shafts at the ends. A lower grip attached to the cross slide. An
upper grip attached to a lever mechanism, which causes a shaft to rotate when load acts
downwards. Counter weights fixed to a pendulum, which swings when shaft rotates. A push
rod with a rack and pinion arrangement to actuate the load scale needle when the push rod is
pressed is by the swinging pendulum. A dashpot to dampen the movement of pendulum. A
rider needle which moves with the load scale needle when the load increases but remains the
last position when the load decreases. A lever with each grip to open and close the vice sothat
the specimen may be inserted into the grip and locked. Two limit switches to cut -off the motor
when the cross slides moves too close to either the base or the upper grip .One push button
each for moving the cross slide up and down and to stop the cross slide. When the motor runs ,
the vertical bolt rotates as a result of which nut moves up or down the bolt. The lower grip also
moves up or down because it is attached to the nut which in turn is welded to the cross slide .
The fixed between the upper and lower grips thus gets loaded or unloaded depending on
whether the lower grip is moving up or down respectively .The lever attached to the upper grip
gets operated due to the load transmission to the upper grip from the lower grip through the
specimen .
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DESCRIPTION OF THE SPECIMEN: Straight piece of uniform cross -section over the test
length . Enlarged ends which can be held . The gauge length to the cross-sectional area is
because % of elongation is not a unique quantity for a material but varies with the gauge length
For this reason gauge length is standardized so that comparison of ductility between two
materials may be made consistently length. Measure the dimensions of the specimen. Press the
lever to open the vice of the upper grip and insert the specimen inside the vice - Then release
the lever to lock the specimen. Move the lower grip up and when the bottom end of the
specimen enters into
PROCEDURE
OBSERVATIONS-
Initial reading on linear scale = Initial reading on load scale = Initial gauge length = Initial dimensions of specimen = Initial area of cross section =
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PRECAUTIONS-
1. Switch on the machine craftily.
2. Fix the specimen at proper position in the machine.
3. Check the specimen should be marked with punch before fix it. 4. Note down the reading of both scales carefully.
5. Switch off the machine after performing the experiment.
TENSILE TEST SPECIMEN
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Graph:-
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RESULT
% OF ELONGATION = % OF REDUCTION IN AREA = TENSILE STRENGTH =
MODULUS OF ELASTICITY =
QUESTIONS:
1. What is engineering stress
2. What is engineering strain 3. What is modulus of rigidity
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4. What is modulus of toughness
5. What is modulus of resistance
6. What is proportional limit
7. What is elastic limit
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8. What is yield point
9. What is proof stress
10. What is ultimate tensile strength
11. What is percentage of reduction and percentage of elongation
12. What is ductility and malleability
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13. How does a mild steel fail?
14. Which instrument is used for measuring elongation within yield point?
15. What is gauge length?
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Experiment No. 2 Name_________________RollNo.________Group/BatchNo.__________
Date_______Marks/Grade__________FacultysSignature____________
Aim:- To perform the compression test on UTM
Theory: - A compression test can be performed on UTM by keeping the test-piece on
base block and moving down the central grip to apply load. It can also be performed on a
compression testing machine. A compression testing machine shown in fig. it has two
compression plates/heads. The upper head moveable while the lower head is stationary.
One of the two heads is equipped with a hemispherical bearing to obtain Uniform
distribution of load over the test-piece ends. A load gauge is fitted for recording the
applied load.
SPECIMEN: - In cylindrical specimen, it is essential to keep h/d = 2 to avoid lateral
instability due to bucking action. Specimen size = h = 2d
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PROCEDURE :-
OBSERVATION :-
1. Initial length or height of specimen h = ------mm
2. Initial diameter of specimen do = -------------mm.
CALCULATION :-
Original cross-section area Ao =
Final cross-section area Af =
Stress =
Strain =
Determine percentage reduction in length (or height) to the specimen
Determine ultimate (max.) compressive strength,
Determine Youngs modulus in compression
PRECAUTIONS:-
The specimen should be prepared in proper dimensions.
The specimen should be properly to get between the compression plates.
Take reading carefully.
After failed specimen stop to m/c.
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Graph
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RESULT:-
CONCLUSION:-
QUESTIONS :-
Q.No. 1 Compression tests are generally performed on brittles materials-why
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Q.No. 2 Which will have a higher strength: a small specimen or a full size member made
of the same material?
Q.No. 3 What is column action? How does the h/d ratio of specimen affect the test result?
Q.No.4 How do ductile and brittle materials in their behavior in compression test ?
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Experiment No. 3
Name__________RollNo._______________Group/BatchNo.__________
Date_______Marks/Grade________FacultysSignature______________
AIM: -To perform the bending test on UTM
APPARATUS USED: - UTM or Beam apparatus, Bending fixture, vernier caliper, meter
rod, test piece & dial gauge
THEORY :- Bending test is perform on beam by using the three point loading system.
The bending fixture is supported on the platform of hydraulic cylinder of the UTM. The
loading is held in the middle cross head. At a particular load the deflection at the center of
the beam is determined by using a dial gauge. The deflection at the beam center is given
by:
EIWLd48
2
PROCEDURE:-
1. Least count of vernier caliper =
2. Length of beam (L) =
3. Width of beam (b) =
4. Thickness of beam (t) ` =
STEPS
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Graph:-
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CALCULATION :-
12
3btI
EIWLd48
2
PRECAUTIONS :-
1. Test piece should be properly touch the fixture
2. Test piece should be straight
3. Take reading carefully
4. Elastic limit of the beam should not be exceeded
RESULT :-
CONCLUSION :-
VIVA-QUESTIONS :-
What is deflection ? how will define ?
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What is moment of inertia?
What is young modulus?
Write Eulers formula
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How many types of column?
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Experiment No. 4
Name_________________RollNo._________Group/BatchNo._________
Date___________Marks/Grade_____FacultysSignature_____________
Aim:- To perform the shearing test on UTM
APPARATUS USED :- A UTM, Specimen, shearing attachment, vernier caliper etc
THEORY :- A type of force which causes or tends to cause two contiguous parts of the
body to slide relative to each other in a direction parallel to their plane of contact is called
the shear force. The stress required to produce fracture in the plane of cross-section, acted
on by the shear force is called shear strength
PROCEDURE :-
OBSERVATION :-
Applied compressive force (F) =
Diameter of specimen =
CALCULATION :-
The shear strength shall be calculated from the following formulae
T= (F/2)/ (pd/4) = 2F/pd
where d is the actual diameter of the specimen
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Graph:-
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PRECAUTIONS :-
1. The specimen should be all place equal dia.
2. Measure the diameter of specimen carefully
3. The specimen should be properly grip between the test rig
4. Take reading more carefully
5. After shearing specimen stop to m/c.
RESULT: - Shear strength of specimen =
CONCLUSION:-
VIVA-QUESTIONS:-
Does the shear failure in wood occur along the 45 shear plane?
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What is single & double shear?
What is find in shear test?
What is unit of shear strength?
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Experiment No. 5
Name_________________RollNo._________Group/BatchNo._________
Date___________Marks/Grade_____FacultysSignature_____________
Aim:- To perform the tensional test on Torsion testing machine
EQUIPMENT REQUIRED - Torsion testing machine, steel rule, micrometer, test piece.
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FIG 2: TORSION TEST SPECIMEN (BEFORE AND AFTER TEST)
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THEORY: A torsion test is performed to determine the modulus of rigidity, torsional yield strength, and modulus of rupture in torsion. The modulus of rupture is equal to the nominal surface stress corresponding to the maximum torque. Now, the torsion formula is given by:
T/J= / R=G/L Where, = Modulus of rupture T == Maximum twisting moment R = Original outer radius of test piece J = Polar moment of inertia = D4 /32, Angle of twist D == Diameter of test piece L = Parallel length of test piece G = Modulus of rigidity Therefore, G=(T/) (L/J) = T x R/ J PROCEDURE
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OBSERVATION:
Diameter of test piece =_____________________________mm Length of the test piece = ____________________________mm
OBSERVATION TABLE:
SNo Torque (Kgfm)
Torque (Nmm)
Angle of twist
(Degree)
Angle of twist
(Radian)
Shear strength (N/ mm2)
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T O R Q U E V S A N G L E O F T W IS T C U R V E
0
1 0
2 0
3 0
4 0
5 0
6 0
7 0
8 0
9 0
1 0 0
0 1 0 2 0 3 0 4 0 5 0 6 0 7 0 8 0 9 0 1 0 0
A N G L E O F T W IS T
TOR
QU
E
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CALCUTATIONS:-
RESULT: Ultimate shear strength = Modulus of rigidity = Modulus of rupture =
PRECAUTIONS: QUESTIONS: 1. What is the purpose of the torsion test?
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2. Define modulus of rigidity? 3. On what factors does the torsional strength of the test piece depends? 4. Under which conditions mild steel and cast iron fails? 5. How wire torsion testing is different from rod testing? 6. Give torsion formula and explain?
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Experiment No. 6 Name_________________RollNo._________Group/BatchNo._________Date__________Marks/Grade____FacultysSignature_______________ AIM: To perform hardness test on hardness test mcahine
EQUIPMENT REQUIRED: Rockwell hardness testing machine, diamond indenter,
Allen key set, specimen to be tested, Brinell attachment.
THEORY: The property of hardness is defined as resistance to indentation or
scratching. Based upon the method of measurement, it can be categorized as follows:
1. Scratch hardness
2. Indentation hardness
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1. BRINELL HARDNESS A steel ball is pressed upon a surface whose hardness to be
measured. This results in an indentation on the surface. The ratio of load, which caused
the indentation to the area of indented surface, is defined as Brinell Hardness Number. If
P = Applied load in kgf
D = Diameter of ball in mm
d = Diameter of indentation in mm
Then
BHN = P / ( D / 2) (D - D2 d2)) kgf / mm2
At any other load the ratio d / D must be constant which requires that P / D2 must be
constant. An anomaly may arise in measurement of diameter of indentation due to
localized deformation of metal in region of indentation. To arrive at the true value of d
the indenter is often coated by a dye before making the indentation. The diameter then
can be measured on the colored ring. To avoid interference between an indentation and
any edge of the specimen, or between two indentations, it is advisable that the center to
edge or center to center distance be at least 1.5 D. Similarly the thickness of plate must be
at least equal to D so that the plastically deformed zone below the indentation does
interfere with the back surface.
2. ROCKWELL HARDNESS In this method two types of indenters are commonly
used.
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1. An indenter in the form of 120o diamond cone
2. Steel balls of 1 / 16- inch and 1/ 8-inch diameters
Rockwell Hardness is measured on an arbitrary scale on which hardness number is
inversely proportionally to depth of indentation. A minor load is applied on the specimen
through the indenter so that the specimen sits properly and tendency for localized
deformation in region of deformation is reduced. Then a major load is applied and the
depth of indentation is automatically recorded as hardness number on a dial gauge. One
combination of load and indenter will not be able to produce a wide range of hardness.
Therefore three loads with three indenters are used in different combinations to provide
wide range to measure hardness of several materials.
The thickness of plate specimen must be at least ten times the depth of indentation
to avoid any effect of indentation to pass through the thickness. The distance between
two adjacent impressions should be at least three times the size of indentation. The
hardness read from indenting the curved surface should be corrected for curvature. The
surface on which indentation is made must be clean and smooth and it should be well
seated upon a clean plate form.
PROCEDURE:
1. BRINELL HARDNESS TEST
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2. ROCKWELL HARDNESS TEST
OBSERVATIONS: ROCKWELL HARDNESS TEST
BRINELL HARDNESS TEST
S.No. Material of specimen Scale used Rockwell Hardness Number
1. 2. 3. 4. 5.
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CALCULATIONS:
S. No. Material of specimen
Applied load
Diameter of ball
Diameter of indentation
Brinell Hardness Number
1. 2. 3. 4. 5.
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RESULT: R.H.N. of material _________________ = R.H.N. of material _________________= R.H.N. of material _________________= B.H.N. of material _________________= B.H.N. of material _________________ = B.H.N. of material _________________ =
PRECAUTIONS:
1. Place the lever at proper position.
2. Clean the surface of specimen with emery paper.
3. Fix the indenter at its position by taking care of diamond tip.
4. Apply and release the major and minor load slowly.
DISCUSSION :
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QUESTIONS:
1. Define hardness? What are the types of hardness tests?
2. What are the ways of conducting indentation tests?
3. What is practical application of hardness test?
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4. What is Brinell hardness number and give value of P and D in Brinell test?
5. What should be the rate of load application in Brinell test and how much time the load be maintained in Brinell test?
6. What is Rockwell Hardness Number and give the standard scales?
7. What is minor load and why it is applied?
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8. What is relation between penetration and reading on scale?
9. How is machine checked for accuracy?
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Experiment No. 7
Name____________________RollNo.______Group/BatchNo._________
Date_________Marks/Grade______FacultysSignature_____________
AIM: To perform toughness test on toughness test machine.
EQUIPMENT REQUIRED: Impact testing machine, specimen to be tested, izod and charpy hammers, steel rule, Leveler.
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THEORY:Brittle fracture tendency in materials like steel develops due to
1. A tri-axial state of stress
2. Low temperature
3. High strain rate.
Stress calculation at the tip of a notch under impact load is extremely difficult, due to
which the results of impact tests are not presented in the form of a stress. The property
that is measured in the impact test is the energy absorbed in fracturing the specimen of
standard dimensions and standard notch. This property measured in Joules is called
impact toughness. Impact toughness is property of specimen and is a good qualitative
index of behavior of material in presence of notch at low temperature. Such an index is
not possible to obtain from any static test; therefore this property is largely used in
selection of material and for development of material for specific purposes of inhibiting
the tendency of brittle fracture. The energy absorbed in fracture decreases as temperature
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decreases. In a particular temperature range the impact toughness decreases sharply with
decrease in temperature. Below this range material behaves in a brittle fashion.
PROCEDURE:
1. Charpy impact test
2.Izod impact test
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OBSERVATION: 1.Izod Test Dimensions of specimen Length = Breadth =
Notch angle and its depth = 2.Charpy Test Dimensions of specimen Length = Breadth = Notch angle and its depth =
S.No. Type of material Total energy J
Loss of energy J
Resultant energy J
1. 2. 3.
S.No. Type of material Total energy J
Loss of energy J
Resultant energy J
1.
2. 3.
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RESULT:
DISCUSSION:
PRECAUTIONS:
QUESTIONS:
1. What is influence of increase in strain rate?
2. What is an impact load?
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3. What property is measured in impact test?
4. What is the principal of impact test energy measurement?
5. Give differences between Izod and Charpy test?
6. What is the purpose of notch in the specimen?
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7. Define notch sensitivity?
8. Describe the surface in brittle failure and ductile failure?
9. What is transition temperature?
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Experiment No. 8 Name___________Roll No._________Group/Batch No._______________
Date________Marks/Grade______FacultysSignature_______________
AIM: To perform fatigue test on fatigue test machine.
EQUIPMENT REQUIRED: Fatigue testing machine, steel rule, micrometer, specimen to be tested, and adjustable spanner THEORY: On repeated application of load for a large number of time, a material fails even if the associate stress is less then the UTS of the material. Even though the load that are imposed upon machine parts and structures in the service may be random the nature, laboratory test are generally performed under sinusoidal stress for convenience. Techniques have been developed to use these result for application under actual service condition. The maximum value of stress is called max . the minimum value of stressis called min . The average value of stress is called m. The amplitude is given by half of the difference between maxand min. When max is zero then the loading is called repeated. When m is zero then the loading is called fully reversed. The ratio of maxand min is called stress ratio. The stress that are applied upon the fatigue test specimen can be axial, banding, torsion or there combination. The minimum value of stress beyond which specimen requires infinite number of cycle to fail is called ENDURANCE LIMIT.
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The fatigue behavior depends upon various factors
1. Frequency:- At high frequency ( above 1000 cycle per mim) , there is improvement in
life because less time is available during a load cycle to extend a crack. Below 200 cycle
per min. fatigue limit tends to become less with lower frequencies. Between 200 to 1000
cycle per min. there is generally no influence on fatigue behavior.
2. Surface condition:- better surface finish, better the fatigue behavior. Surface treatment
also increase fatigue life.
3. Stress concentration:- the fatigue strength decrease in presence of stress
concentration.
PROCEDURE:-
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OBSERVATION:- Weight used (W) =
Distance between fixed end and the end to witch weight is suspend (free
end) =
Diameter of rod first portion of specimen (d) =
Diameter of end portion of specimen (D) =
Moment of force (M) = W x L =
Stress (S) =
Number of cycle (N) =
CONCULATION:- RESULT:-
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QUESTION:- 1. What is fatigue? 2. Explain factor effecting fatigue 3. Explain endurance limit. 4. What is infinite number of cycle?
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Experiment No. 9 Name___________Roll No._________Group/Batch No._______________
Date________Marks/Grade______FacultysSignature_______________
AIM: To perform cupping test on cupping test machine.
EQUIPMENT REQUIRED: Erichsen cupping testing machine, sheet to be tested, Steel
rule.
THEORY:
The test consists of clamping a metal test piece under controlled pressure between
a retaining ring and pressing the test piece into the die by means of a ball or penetrater
having a spherical head until ruptures commences .The depth of penetration thereby
obtained is measured and provides an indication of the stretch forming capacity of the
sheet or strip within the limits imposed by the conditions of the test .
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PROCEDURE:
OBSERVATION:
S.No.
Type of metal
Thickness of sheet (mm)
Initial reading of dial gauge
Final reading of dial gauge
Cupping umber
(from table)
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CALCULATIONS:
RESULT:
cupping value of the specimen No._______________ =
cupping value of the specimen No._______________ =
cupping value of the specimen No._______________ =
PRECAUTIONS:
1. The test piece should be flat and thickness should not be more than 2 mm.
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2. The grease should be applied at the point of contact on the specimen.
3. The force should be applied slowly and constantly on the lever.
4. The reading of dial gauge should be taken carefully.
5.
SHORT QUESTIONS:
1. What is cupping number?
2. What is importance of cupping test?
3. What is drawing and deep drawing?
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4. Give some example of other forming operations?
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CUPPING NUMBER TABLE
MINIMUM ERICHSEN VALUES OF SHEET
THICKNESS IN mm CUPPING DEPTH IN mm (min)
TYPE D TYPE DD TYPE EDD 0.50 8.34 8.80 9.20 0.55 8.40 8.94 9.36 0.60 8.56 9.10 9.50 0.65 8.72 9.22 9.64 0.70 8.98 9.38 9.78 0.75 9.04 9.51 9.92 0.80 9.20 9.66 9.04 0.85 9.34 9.80 9.20 0.90 9.50 9.94 9.32 0.95 9.62 10.06 9.48 1.00 9.80 10.20 10.58 1.05 9.94 10.32 10.70 1.10 10.08 10.46 10.84 1.15 10.20 10.58 10.95 1.20 10.35 10.70 11.06 1.25 10.44 10.82 11.15 1.30 10.58 10.94 11.25 1.35 10.70 11.03 11.35 1.40 10.80 11.12 11.44 1.45 10.90 11.22 11.53 1.50 11.00 11.30 11.64 1.55 11.08 11.35 11.72 1.60 11.14 11.40 11.80 1.65 11.18 11.46 11.88 1.70 11.24 11.52 11.94 1.75 11.26 11.57 12.02 1.80 11.30 11.62 12.08 1.85 11.30 11.66 12.14 1.90 11.30 11.72 12.20 1.95 11.29 11.76 12.26 2.00 11.28 11.80 12.3
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Experiment No. 10 Name_______________RollNo._________Group/Batch No.__________
Date__________Marks/Grade____FacultysSignature_______________
Aim: To study the behavior of column with various end conditions.
Apparatus Equipment:
Column buckling apparatus, weights, vernier calliper, screw gauge, weight container, etc.
Theory:
If compressive load is applied on a column, the member may fail either by crushing or by
buckling, depending upon its material, cross section and length. If member is
considerably long in comparison to its lateral dimensions, it will fail by bucking. If a
member shows signs of buckling, the member leads to failure with small increase in load.
The load at which the member just buckles is called buckling or critical load. For a
slender column, buckling load is less than the crushing load. The buckling load, as given
by Euler, can be found by using following expression:
Where E = Modulus of elasticity = 2.0 x 105 N/mm2 for steel
I = Least moment of inertia of column section
1e = Effective length of column
P = Critical or buckling load
Depending on support conditions, four cases may arise. The effective length for each of
which are given as under
Both ends are fixed
2Lle
One end is fixed and other is pinned
2Lle
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Both ends are pinned
Lle
One end is fixed and other is free
Lle 2
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Apparatus consists of four spring steel columns, which are put along a vertical wooden
board. These four columns have different end conditions as below:
Both ends fixed
One end fixed and the other pinned
Both ends pinned
One end fixed and other end free
Suggested Experimental Work:
Step1: Pin a graph paper on the wooden board behind the column.
Step2: Apply the load at the top of columns increasing the gradually. At certain stage of
loading the columns shows abnormal deflections and the gives the buckling load.
Step3: Note the buckling load for each of the four columns.
Step4: Trace the deflected shapes of the columns over the paper. Mark the points of
change of curvature of the curves and measure the effective length for each case
separately.
Step5: Also calculate the theoretical effective lengths and thus buckling loads by the
expressions given above and compare them with the observed values.
Results and Discussions:
1) Calculate the Euler's buckling load for each case.
2) Also calculate the theoretical effective lengths and thus buckling loads by the
expressions given above and compare them with the observed values.
Sample Data Sheet:
Width of strip (mm) b=
Thickness of strip (mm) t=
Length of strip (mm) L=
Least moment of inertia 12
3btI
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PROCEDURE:-
CALCULATION:-
Sl.
No
End conditions Eulers
Buckling load (kg)
Effective
Length (mm)
Theoretical Observed Theoretical Observed
1.
2.
3.
4
Both ends fixed
One end fixed and the
Other pinned
Both ends pinned
One end fixed and the
other free.
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Results and Comments:
Questions:
1. What is equivalent length
2. Define buckling and Crushing.
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Experiment No. 11 Name________________Roll No.________Group/Batch No.__________
Date _________Marks/Grade____Facultys Signature_______________
Aim:- To verify the moment area theorem regarding the slopes and deflections of the
beam
Equipment required
Apparatus of Elastic properties of beam, weights, dial gauge, meter scale, etc.
Theory:
According to moment area theorem:
1. The change of slope of the tangents of the elastic curve between any two points of the
deflected beam is equal to the area of EIM diagram between these two points.
2. The deflection of any point relative to tangent at any other point is equal to the moment
of the area of theEIM diagram between the two points about the point at which the
deflection is required.
Slope at bYB 2
Since the tangent at C is horizontal due to symmetry,
Slope at EI
B area shaded
aLWaWa
EI 221 2
Displacement at B with respect to tangent at C
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(y1 + y2)= EI
Babout area shaded ofMoment
=
42232
21 LabaLWaabaWa
EI
Procedure:
Length of main span, L (cm) =
Length of overhang on each side, a (cm) =
Modulus of elasticity, E (kg/cm2) calculated = 2.1 x 106
Steps:-
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Sl. No. Load
at each
hanger
(kg)
Central
Deflection y1
(cm)
Deflection at
free end y2
(cm)
Slope at B
by2
Deflection at C
(y1) cm = &
Deflection at B
(y2) cm =
Results and Discussions:
1. Calculate the slope at B as by2 (measured value).
2. Compute slope and deflection at B theoretically from B. M. D. and compare with
experimental values.
3. Deflection at C = y1 (Measured value)
4. Deflection at C = Average calculated value
Comments:
The moment area theorems may often be used more conveniently in the computation of
slopes and
Deflection of beams and frames, practically when concentrated rather than distributed
loads cause the deformation. These theorems are based on a consideration of the
geometry of the elastic curve of the beam and the relation between the rate of change of
slope and the bending moment at a point on the elastic curve.
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Precautions:
Apply the concentration loads without jerks.
Measures the deflection only when the beam attains equilibrium.
Measure deflection very carefully and accurately.
Check the accuracy and least count of dial gauges used for measuring deflections.
Figures:
Calculations:
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Results and Comments:
Questions:
1. State moment area theorem
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2. Where moment area theorem can be applied
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Experiment No. 12 Name___________Roll No._________Group/Batch No._______________
Date________Marks/Grade______FacultysSignature_______________
Aim: To determine the elastic properties of beam.
Equipment required:
Apparatus of Elastic properties of beam, weights, dial gauge, meter scale, etc.
Theory:
For the beam with two equal overhangs and subjected to two concentrated loads W each
at the free
ends, the maximum deflection y at the centre is given by
Central upward deflection, EILawy
8.. 2
1
Where,
a = length of overhang on each side
W = load applied at the free ends
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L = main span
E = modulus of elasticity of the material of the beam
I = moment of inertia of cross section of the beam
yLawEI
8.. 2
2
Also it is known that EI for beam = 12 bd3 x E
3
where, b = width of beam
d = depth of bean
Procedure:
Observation Table:
Length of main span, L (cm) =
Length of overhang on each side, a (cm) =
Width of beam, b (cm) =
Depth of beam, d (cm ) =
Modulus of elasticity, E (kg/cm2) = 2.1 x 106
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Results and Discussions:
1. Calculate the experimental value of EI by Eq. (2).
2. Compare the experimental value of EI with theoretical values.
Average values of EI from observation = ---------- kg. sq.cm
Average values of EI from calculation = ------------ kg.sq. cm
Comments:
Precaution:
Measure the central deflection y very accurately.
Ensure that the beam is devoid of initial curvature.
Loading should be within the elastic limit of the materials.
Sl. No. Equal loads at
the two ends
(kg)
Dial gauge reading at
the midspan of
beam(cm)
EI fromEq. (3)
(Kg.Sq. cm)
EI fromEq.(2)
(Kg. Sq. cm )
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Figures:
Calculations:
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Results and Comments:
Questions:
What is flexural stiffness?
What is the value of EI for any beam?