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Apr 3, 2024
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University of Wisconsin-Milwaukee Civil Engineering 203 Introduction to Solid Mechanics Laboratory Manual 2022
CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 i CONTENTS Laboratory Report Format ..............................................................................................................
1
I.
Title Page ......................................................................................................................
1
II.
Objective .......................................................................................................................
1
III.
Questions
.......................................................................................................................
1
IV.
Conclusions ...................................................................................................................
1
V.
References .....................................................................................................................
1
Additional Formatting Guidelines ..................................................................................................
2
I.
General ..........................................................................................................................
2
II.
Values ...........................................................................................................................
2
III.
Calculations
...................................................................................................................
2
IV.
Data ...............................................................................................................................
3
V.
Tables ............................................................................................................................
3
VI.
Graphs ...........................................................................................................................
3
VII.
Conclusions ...................................................................................................................
4
VIII.
References .....................................................................................................................
4
Lab #1: Stress Strain Curves of Steel and Aluminum in Tension ..................................................
5
I.
I. Objective and Background ........................................................................................
5
A.
Terminology .......................................................................................................
5
II.
Laboratory Procedure
....................................................................................................
7
III.
Recorded Data ...............................................................................................................
9
A.
Tension Test of Steel ..........................................................................................
9
B.
Tension Test of Aluminum .................................................................................
9
IV.
Questions
.......................................................................................................................
9
V.
Conclusions .................................................................................................................
10
VI.
References ...................................................................................................................
10
Lab #2: Stress Strain Curves of Concrete and Wood in Compression .........................................
11
I.
Objective and Background ..........................................................................................
11
A.
Terminology .....................................................................................................
11
II.
Laboratory Procedure
..................................................................................................
12
III.
Recorded Data .............................................................................................................
13
IV.
Questions
.....................................................................................................................
16
V.
Conclusions .................................................................................................................
16
VI.
References ...................................................................................................................
16
Lab #3: Stress Concentrations ......................................................................................................
17
I.
Objective and Background ..........................................................................................
17
A.
Terminology .....................................................................................................
18
II.
Laboratory Procedure
..................................................................................................
18
III.
Recorded Data .............................................................................................................
20
IV.
Questions
.....................................................................................................................
21
V.
Conclusions .................................................................................................................
24
VI.
References ...................................................................................................................
24
Lab #4: Torsion Test for Material Properties in Shear .................................................................
25
CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 ii I.
Objective and Background ..........................................................................................
25
A.
Terminology .....................................................................................................
26
II.
Laboratory Procedure
..................................................................................................
27
III.
Recorded Data .............................................................................................................
28
IV.
Results and Calculations .............................................................................................
29
V.
Conclusions .................................................................................................................
30
VI.
References ...................................................................................................................
30
Lab #5: Flexure of Beams .............................................................................................................
31
I.
Objective and Background ..........................................................................................
31
A.
Terminology .....................................................................................................
31
II.
Laboratory Procedure
..................................................................................................
31
III.
Recorded Data .............................................................................................................
32
IV.
Questions
.....................................................................................................................
33
Appendix A ...................................................................................................................................
36
I.
Factorial Design of Experiments ................................................................................
36
A.
Response ...........................................................................................................
36
B.
Factors ..............................................................................................................
36
C.
Levels ...............................................................................................................
36
D.
Null Outcome ...................................................................................................
36
E.
Main Effects .....................................................................................................
36
F.
Interaction Effects ............................................................................................
36
II.
2
k
Factorial Design of Experiments ............................................................................
37
III.
2
2
Factorial Design of Experiments ............................................................................
37
IV.
Statistical Analysis ......................................................................................................
37
V.
Conclusions .................................................................................................................
37
VI.
References ...................................................................................................................
37
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CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 1 of 36 LABORATORY REPORT FORMAT I.
Title Page Include Name and Number of Lab, Your Name, and the Date II.
Objective Write a brief (1-2 sentences) statement of the objectives and key concepts of the lab. Please write this in your own words and do not copy directly from the lab manual. III.
Questions Answer each question in the “Calculations” section of the laboratory manual. Please number each question as in the lab manual
, and leave adequate space between questions to distinguish one question and answer from the next. Usually, some questions will ask for “data,” so you do not need to have a separate section on data. SHOW ALL WORK for each problem. In some cases, it may be appropriate to generate calculations with a spreadsheet in which the same calculation is repeated many times. In such cases, show a sample calculation and explain how you encoded the spreadsheet formulae. IV.
Conclusions Summarize what the basic results of the lab were, what errors may have occurred, what you learned, whether the experimental results were expected, and what new questions you have. You must supply evidence for your reasons. For example, a statement such as “I think that human error was responsible for some of our errors” is insufficient. You should explain which human error affected which measurement, and how significant the error was by providing an error analysis computation. V.
References Cite any sources you referenced. All citations must include at least Title, Author, Publisher, and Date. Bare URLs are never sufficient.
CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 2 of 36 ADDITIONAL FORMATTING GUIDELINES I.
General Format your lab reports with a word processor, use a spreadsheet or similar program to report data, and generate graphs electronically. If you are neat, you may hand write your sample calculations. Please see the instructor if you need assistance using electronic formatting. Work in groups of 3-4, and hand in single lab report per group. Each group should have at least one person who is skilled with Excel or some other data-processing software. The laboratory manual has been carefully written to alert you to which data is “recorded,” and which is “calculated.” Please be clear about this when you do your labs. II.
Values If you are reporting some value, such as yield stress, that might have already been published elsewhere, you should also include that published number, with a suitable reference, and discuss how the number you measure or calculate compares to the published value. If you refer to a published number, you should show what that number is and provide a valid reference for it. An extremely useful comparison is percent difference. III.
Calculations All calculations performed should be demonstrated with symbols and then sample numbers from the data you collect, as shown below Stress:
2
2
4
4
100 lb
2037 psi
0.25 in
F
F
A
d
If you cannot use an equation editor, as in the example above, then in many cases, especially with fractions, neat hand writing is preferable to simply entering the equation in one long single line. For example, consider the following, equivalent statements: A. (123 lb + 127 lb)/((0.5 in)(0.5 in)) = 500 lb/in^2 B. 2
123 lb
127lb
lb
500
(0.5in.)(0.5in.)
in
Each is correct, but A is more difficult to read. You are encouraged to write in the style B. You may do this either by handwriting or using the equation editor. Note that in all cases, variables should be in italics, but numbers, mathematical operators (
x
, +, etc.), parentheses, and units should not be italicized.
CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 3 of 36 As a rule of thumb, the reader should be able to reproduce each of your calculations easily from your examples. IV.
Data Do not show the numbers of machine recorded data, such as force and displacement automatically recorded every second by the Instron testing machine. Instead, they belong in a graph. Any number that you collect by hand, that is you see it with your eyes and record it with your hand and a writing implement or a keyboard, should be displayed in the report. You must know and include the units for the data that you use. If the machine records force in pounds, and you treat it as stress in psi, you are creating gibberish. V.
Tables By the time you include 3 numbers in a sentence, such as the yield stress of aluminum, brass, and steel, you should take them out and put them in a table. To the extent possible and practical, combine separate tables of similar values, such as yield stress and failure stress for different materials into a single table. This facilitates comparisons and improves comprehension for the reader and the writer. Tables should have a 2D arrangement of values. Listing all the numbers in a single column makes them nearly as difficult to read as they were when they were in a sentence. Units should not take up an entire row or column of a table. Include them in a column or row title. For example: Poor example section material value Units 011 brass 0.125 in. steel 0.124 in. 012 brass 0.123 in. steel 0.125 in. 013 brass 0.127 in. steel 0.126 in. Good example section brass (in.) steel (in.) 011 0.125 0.124 012 0.123 0.125 013 0.127 0.126 In reporting data, you should be consistent with the precision, lining up all decimal points. This may violate principles of significant figures in some cases, but it vastly improves readability and facilitates comparisons. VI.
Graphs Always graph the independent variable on the horizontal axis and the dependent variable, the variable that depends upon the independent variable, on the vertical axis. For example, in the case of stress vs strain, the Instron machine creates a deflection that you specify and from which you calculate strain, and then it measures the force created by that deflection, from which you calculate stress. Thus, strain is the independent variable that belongs on the horizontal axis, and stress is the dependent variable that belongs on the vertical axis.
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CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 4 of 36 All graphs should have a title, and both axes should have labels that indicate the variable or property plotted along that axis units of that variable or property. Any graph with only one set of data should not have a legend, even though the default Excel behavior is to show a legend. If the legend contains only one entry, you should delete it. Figure 1: Example stress strain curves If the property being plotted could reasonably be interpolated between two data points, such as with deflection under load, connect them with straight lines that go through all data points. If not, as some property you measure from similar samples, do not. For example, it is reasonable to assume that the stress value for the strain 0.015 lies somewhere between the stress values for strains of 0.01 and 0.02, but it is not reasonable to assume that the diameter of sample 1.5 lies between the diameters of samples 1 and 2. The former should be graphed as a lines, and the later should be graphed as points. Resize the default Excel symbol to be small enough to allow distinguishing data points. Pick different symbols so that different data sets can be distinguished on the same graph in black and white, if you are going to print your report in black and white. Do not show Excel’s canned trend line equation. It is not Young’s Modulus or whatever else you might be trying to convey. With a y
intercept and no units, it is merely gibberish. VII.
Conclusions Do not simply state what your values are and what someone else’s values are. This belongs in a table, ideally with a percent difference, and then it can be found there. Instead, you should discuss similarities and differences, and explain why they exist and/or what they mean. VIII.
References If you report a number that you did not record or did not calculate from numbers you recorded, you must indicate where you found it. 0
10000
20000
30000
40000
50000
60000
0
0.02
0.04
0.06
0.08
0.1
Stress (psi)
Strain (in./in.)
Aluminum
Tue 8 am
Tue 11 am
Thur 8 am
Thu 11 am
0.2% offset
CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 5 of 36 LAB #1: STRESS STRAIN CURVES OF STEEL AND ALUMINUM IN TENSION I.
I. Objective and Background The objective of this lab is to determine basic mechanical properties of steel and aluminum. Many important engineering material properties can be determined by testing materials and generating stress-strain curves. In this set of experiments, we will generate stress-
strain curves by applying and measuring axial force and displacement. While a variety of test methods and specimen types exist for obtaining these values, all methods share some basic features. First, there must be a means of applying and measuring axial load to a test specimen. The engineering stress
can then be computed as the axial load divided by the cross sectional area of the original specimen. Second, the change of length of the specimen must be measured. Then the strain can be calculated as the change in length (
deformation
) divided by the initial length of the specimen. Since strains are typically very small quantities, it is necessary sometimes to take average measurements over long specimens. Some important engineering material properties, such as the Young’s Modulus (modulus of elasticity) are measured from data points at which the strain is very small. Other material properties are measured from data points at which the strain is very large. For example, the strain at which the material ruptures may be several hundred times larger than the strains used to measure the modulus of elasticity. Therefore, it is often necessary to generate at least two stress-strain plots to display fully all of the critical details of the material behavior. One plot would detail small strain measurements, while the other would detail measurements at larger strains. A.
Terminology Proportional Limit:
Farthest point on stress-strain curve to which proportionality of stress and strain extends. Modulus of Elasticity:
Slope of proportional or the linear part of the Stress vs. Strain curve. Calculated as E
=
/
, were E
= modulus of elasticity,
= stress up to the proportional limit, and
= strain up to the proportional limit. Yield Point:
Point at which there begins to be an appreciable yielding of the material without any corresponding increase of load. The yield point is sometimes identifiable by a sharp corner in the stress-strain diagram. However, if no such point exists, draw a line with slope E
through the point 0.2% (or 0.002 in./in.) on the strain axis. The yield point is where this line intersects the stress-strain curve. Ultimate Stress:
Largest (engineering) stress experienced by test specimen.
CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 6 of 36 Point of Fracture:
Point at which test specimen ruptures mechanically. Modulus Of Resilience:
Partial area under stress-strain curve up to the proportional limit. It represents the energy that can be absorbed per unit volume without creating a permanent distortion. Modulus of Rupture:
Amount of energy required to cause mechanical rupture of specimen. It is equal to the area under the entire stress-strain curve. Percent Elongation = Δ
L
% = [(
L
f
– L
0
)/
L
0
] x
100%
Percent Reduction = Δ
A
% = [(
A
0
– A
f
)/
A
0
] x
100% Figure 1: Example stress strain curves for different materials Stress
Strain
Stress vs. Strain
(aluminum)
Proportional Limit
0.2%
Yield Point
Point of Fracture
(Ultimate Stress)
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CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 7 of 36 II.
Laboratory Procedure The following table and figures summarize the materials, specimen sizes, and instrumentation that will be used in this lab. The accompanying figures display images of the specimens and some testing equipment. Figure 2: INSTRON Testing Machine Figure 3: Standard Dimensions of Steel Sample Used in Tensile Test Figure 4: Standard Dimensions of Aluminum Sample Used in Tensile Test For both steel and aluminum, inscribe gage marks onto the sample using the punching device. Next, measure the original width, diameter or thickness and gage length of the test sample. Mount the specimen between the two grips of the INSTRON testing machine. To start the test use Instron Bluehill Software as directed by your lab instructor. The output displacement and force data will be saved in a comma separated values file (.csv), keep a copy of this file for future data processing. Testing Machine INSTRON 3369 Capacity 11K Measuring Device Load Cell Gage Length 2"
CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 8 of 36 Figure 5: Electronic Extensometer Figure 6: Steel Tensile Test Setup Figure 7: Aluminum Tensile Test Setup Figure 8: Ruptured Aluminum Specimen
CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 9 of 36 Figure 9: Sample Stress-Strain Diagram: III.
Recorded Data A.
Tension Test of Steel Measurement Initial Final Thickness Width Gage Length B.
Tension Test of Aluminum Measurement Initial Final Diameter Gage Length IV.
Questions SHOW ALL WORK AS DESCRIBED IN LAB FORMAT 1.
Stress-Strain Curves (Steel and Aluminum)
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CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 10 of 36 a.
Send a digital copy of the data recorded to your instructor. b.
Calculate stress-strain values from the recorded data (note that a reasonable conversion factor may be needed to obtain a correct diagram, your instructor should provide you with an actual stress-strain data that you will use to find this factor.) c.
Plot the Stress-Strain Diagram and show the following items on it: Yield Stress, Proportional Limit, Ultimate Strength, Breaking Stress, Moduli of Elasticity, Resilience and Rupture. 2.
Using the data you collected in the lab, complete the following chart of mechanical properties. Show all work, but also summarize all results in a chart of this format. In particular, clearly describe which data points you are using to base your calculations. Aluminum Steel Proportional Limit Yield Strength Ultimate Strength Modulus of Elasticity Modulus of Resilience Modulus of Rupture Percent Elongation Percent Area Reduction 3.
Which material will deform the most if stressed to 50% of its yield strength? How is this conclusion reached? V.
Conclusions Write a concluding statement according to the lab format guidelines. VI.
References
CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 11 of 36 LAB #2: STRESS STRAIN CURVES OF CONCRETE AND WOOD IN COMPRESSION I.
Objective and Background The objective of this lab is to determine basic mechanical properties of wood and concrete. Many important engineering material properties can be determined by testing materials and generating stress-strain curves. In this set of experiments, we will generate stress-
strain curves by applying and measuring axial force and displacement. While a variety of test methods and specimen types exist for obtaining these values, all methods share some basic features. First, there must be a means of applying and measuring axial load to a test specimen. The engineering stress
can then be computed as the axial load divided by the cross sectional area of the original specimen. Second, the change of length of the specimen must be measured. Then the strain can be calculated as the change in length (
deformation
) divided by the initial length of the specimen. Since strains are typically very small quantities, it is necessary to sometimes take average measurements over long specimens. Some important engineering material properties, such as the Young’s Modulus (modulus of elasticity) are measured from data points at which the strain is very small. Other material properties are measured from data points at which the strain is very large. For example, the strain at which the material ruptures may be several hundred times larger than the strains used to measure the modulus of elasticity. Therefore, it is often necessary to generate at least two stress-strain plots is necessary to fully display all of the critical details of the material behavior. One plot would detail small strain measurements, while the other would detail measurements at larger strains. A.
Terminology Proportional Limit:
Farthest point on stress-strain curve to which proportionality of stress and strain extends. Modulus of Elasticity:
Slope of proportional or the linear part of the Stress vs. Strain curve. Calculated as E
=
/
, were E
= modulus of elasticity,
= stress up to the proportional limit, and
= strain up to the proportional limit. Yield Point:
Point at which there begins to be an appreciable yielding of the material without any corresponding increase of load. The yield point is sometimes identifiable by a sharp corner in the stress-strain diagram. However, if no such point exists, draw a line with slope E
through the point 0.2% (or 0.002 in./in.) on the strain axis. The yield point is where this line intersects the stress-strain curve. Ultimate Stress:
Largest (engineering) stress experienced by test specimen.
CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 12 of 36 Point of Fracture:
Point at which test specimen ruptures mechanically. Modulus Of Resilience:
Partial area under stress-strain curve up to the proportional limit. It represents the energy that can be absorbed per unit volume without creating a permanent distortion. Modulus of Rupture:
Amount of energy required to cause mechanical rupture of specimen. It is equal to the area under the entire stress-strain curve. II.
Laboratory Procedure The following table and figures summarize the materials, specimen sizes, and instrumentation that will be used in this lab. The accompanying figures display images of the specimens and some testing equipment. Figure 1: Tinius Olsen Testing Machine Figure 2: Wood Sample Dial Indicator Figure 3: Concrete Sample Dial Indicator Testing Machine Tinius Olsen Capacity 400 K Measuring Device Dial Indicator/ Load Cell Gage Length 6”
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CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 13 of 36 Figure 4: Standard Dimensions of Wood Sample Used in Compression Test Figure 5: Standard Dimensions of Concrete Sample Used in Compression Test Record dial indicator reading at zero load for the sample. Begin to apply load. Record the dial readings on both sides of the specimen at intervals of 10,000 lb for the concrete and 2500 lb for the wood. Repeat this process until the instructor has determined that it is no longer safe to conduct this experiment with the dial indicators mounted on the sample. Remove the dial indicators, so that they are not damaged, and continue to increase load on the sample until failure
.
The maximum load at failure should be recorded. III.
Recorded Data Record the data from the lab in the tables given on the following pages. Be sure to note that much of the data in the tables is calculated, and not recorded. 12 in. 6 in. Gage length 2.5 in. 2.5 in. 12 in. 6 in. 6 in. Gage length 6 in.
CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 14 of 36 Compression Test of Wood General Data Sample length Gage length: Cross section width Cross section area Ultimate load: 1 2 3 4 5 6 7 8 Load (lb) Displacement Readings (in.) Displacement Readings (Absolute) (in.) Avg Disp. δ
avg (in.) Stress σ
(psi) Strain
(
μ
in./in.) Front Rear Front Rear 0 0 0 -- 0 0 2500 5000 7500 10000 12500 15000 17500 20000 22500 25000 27500 30000 32500 35000
= δ
avg /6" and σ
= P/A
0
Notes:
Data is recorded in columns 1-3 and calculated in the rest.
The absolute displacement is determined by subtracting the first reading from all other readings.
CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 15 of 36 Compression Test of Concrete General Data Sample length Gage length: Diameter Cross section area Ultimate load: 1 2 3 4 5 6 7 8 Load (kip) Displacement Readings (in.) Displacement Readings (Absolute) (in.) Avg Disp. δ
avg (in.) Stress σ
(psi) Strain
(
μ
in./in.) Front Rear Front Rear 0 0 0 -- 0 0 10 20 30 40 50 60 70 80 90 100 110 120 130 140 150
= δ
avg /6" and σ
= P/A
0
Notes:
Data is recorded in columns 1-3 and calculated in the rest.
The absolute displacement is determined by subtracting the first reading from all other readings.
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CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 16 of 36 IV.
Questions SHOW ALL WORK AS DESCRIBED IN LAB FORMAT 1.
Stress-Strain Curves (Wood) a.
Provide a copy of the data tables recorded and calculated for both concrete and wood. Remember that you need to show, at least, a sample calculation of everything you do. b.
Plot the Stress-Strain Diagram and show the following items on it: Yield Stress, Ultimate Strength, Breaking Stress, Moduli of Elasticity, Resilience and Rupture. Note: use the 0.2% offset method to find the yield stress. 2.
Using the data you collected in the lab, complete the following chart of mechanical properties. Show all work, but also summarize all results in a chart of this format. In particular, clearly describe which data points you are using to base your calculations. Wood Concrete Yield Strength Ultimate Strength Modulus of Elasticity Modulus of Resilience Modulus of Rupture 3.
Which material will deform the most if stressed to 50% of its yield strength? How is this conclusion reached? V.
Conclusions Write a concluding statement according to the lab format guidelines. VI.
References
CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 17 of 36 LAB #3: STRESS CONCENTRATIONS I.
Objective and Background The purpose of this lab experiment is to determine changes in the stress level caused by geometric irregularities such as notches and holes in an axially loaded bar (Figure 1). If a solid plate of constant cross section is loaded along its axis with a force P
, the state of stress in the plate at points away from the ends is uniaxial
. The stress distribution is uniform at any cross section, and has value
= P/A
. For sufficiently small strain, Hooke’s Law can be used to relate stress and strain:
=
E
,
=
/E
When a geometric discontinuity is present, e.g.
a hole or a fillet is cut out from the plate as shown in the plate below; a rise in stress develops in the immediate vicinity of the hole and the fillet. The state of stress near the fillet and hole becomes biaxial
, and the relations between stress and strain are now the following (plane stress case): )
(
1
2
y
x
x
E
, )
(
1
y
x
x
E
)
(
1
2
y
x
y
E
, )
(
1
x
y
y
E
Sample Material Steel Testing Machine INSTRON 3369 Capacity 11K Measuring Device Load Cell Figure 1 Standard Dimensions of the Steel Sample and Location of Gages r
= 0.5 in. r = 0.25 in. 2 in. 0.25 in. z y x 2 1 3 4 5 6 8 7 9 10
CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 18 of 36 A.
Terminology Modulus of Elasticity:
Slope of proportional or the linear part of the Stress vs. Strain curve. Calculated as E
=
/
, were E
= modulus of elasticity,
= stress up to the proportional limit, and
= strain up to the proportional limit. Poisson’s ratio:
The ratio of the lateral strain to the axial strain, in a state of uniaxial
stress: Calculated as ν
= (–lateral strain)/(axial strain) By including the negative sign in the formula, materials that laterally contract under axial extension will have a positive Poisson ratio, and this is the common case. However, some materials have negative Poisson’s ratio. Stress Concentration Factor:
The ratio of the maximum stress to the nominal stress around a discontinuity. Calculated as K
=
max
/
ave
where
max
= maximum stress at the vicinity of the discontinuity,
ave
= the stress obtained by dividing the force by the net cross-sectional area at the discontinuity (location of minimum area), and
nom
= nominal uniform stress away from any discontinuity (at wide portion of material). II.
Laboratory Procedure Strain gages are mounted at 10 locations on a steel specimen as shown in Figure 1. The specimen is placed in the Instron machine and loaded in tension. The strain at each strain gage location must be read and recorded using a Strain Indicator and a Switch and Balance Unit (Figures 4 and 5). Figure 2 Instron Testing Machine Figure 3 Strain Gages
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CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 19 of 36 Figure 4 Switch and Balance Unit Figure 5 Strain Indicator Record your data in the following pages and answer the related questions. Channel Selection
: select the gage number to display in the Strain Indicator. Gage Connection
: connect each strain gage to the correct row number (see Figure 1), in the following sequence: red to red, white to white, and black to yellow. The strain indicator shows the strain in the strain gage selected by Channel Selection switch on the Switch and Balance Unit.
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CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 20 of 36 III.
Recorded Data Applied Load: P
= ______________ lb Gage # Reading w/o Load Reading w/ Load Uniaxial or Biaxial Stress? ε
x
ε
y
σ
x
σ
y
1 2 3 4 5 6 7 8 9 10 Notes:
Data in columns 2-3 is recorded.
The strain reading before applying the load; need not be recorded if the strain is initially balanced.
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CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 21 of 36 IV.
Questions 1.
a.
Determine E
and
by using data from points located far away from any discontinuities. 2
1
strain at gage 2
strain at gage 1
1
1
2
2
Stress
Average of strain at gages 1 & 3
E
0
Load
Cross-section away from discontinuities
P
A
b.
How do the experimental values for Poisson’s Ratio and Modulus of Elasticity compare with the usual accepted values for steel (use standard book values, such as from the textbook)? c.
Explain why you were asked to calculate the values for the material properties at locations far away from the geometric discontinuities. 2.
Complete the data table, providing your recorded data (columns 2-3) and the calculated stresses and strains. Be sure to show your supporting calculations elsewhere, or build a spreadsheet and explain the formulae in your cells. In calculating your strains and stresses, you should first determine the state of stress at each location (column 4). Some locations can be assumed to have a state of uniaxial stress (along the x
-axis), and others should be assumed to have a state of biaxial stress (in the x-y
plane). You should provide an explanation for your assessments of each point, although you may use the fact that the same reasoning may apply to several points. Once you have determined the appropriate state of stress at each location, you can determine the strains and stresses by applying either the 1D (uniaxial) or 2D (biaxial) Hooke’s Law equations, as appropriate: i.
1D Hooke’s Law x
x
E
x
y
ii.
2D Hooke’s Law )
(
1
2
y
x
x
E
)
(
1
y
x
x
E
)
(
1
2
y
x
y
E
)
(
1
x
y
y
E
Note: A zero stress in a given direction does not necessarily imply that the strain in that direction is zero. Similarly, if the strain in a given direction is zero, the stress in that direction is not necessarily zero.
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CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 22 of 36 3.
Determine K
experimental values a.
For the 1" diameter hole: avg
min
P
A
A
min
= shaded area cross-sectional
avg = Average of the stress values calculated from gages 5 and 6 b.
For the 1/4" radius notch: avg
min
P
A
A
min
= shaded area cross-sectional
max = Average of the stress values calculated from gages 9 and 10 4.
Determine the relative Error (based on theoretical) of the K values exp
theoretical
theoretical
%Error
100%
K
K
K
a.
Find K
theoretical
values for the circular hole using Figure 6: 0.25 in. 0.5 in. 0.5 in. 1.0 in. 0.25 in. 1.5 in.
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CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 23 of 36 Figure 6 Stress Concentration Factor Curve for Circular Hole b.
Find K
theoretical
values for notches using Figure 7: Figure 7 Stress Concentration Factor Curve for Notch 5.
Using your data, plot the stress distribution across the section through the large hole. Superimpose a plot of the average stress distribution at that section. 6.
Why is
z
exactly zero on the outside surfaces that are normal to the z-direction? Does the thickness of the specimen matter? 7.
The 3D stress-strain relation for strain in the z
-direction across the thickness is given as follows: )
(
1
y
x
z
z
E
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CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 24 of 36 What is the strain
z at the location of the gages 7 and 8? Explain the physical meaning of this strain. V.
Conclusions Write a concluding statement according to the lab format guidelines. VI.
References
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CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 25 of 36 LAB #4: TORSION TEST FOR MATERIAL PROPERTIES IN SHEAR I.
Objective and Background The objective of this lab is to determine shear properties of 1020 Hot Rolled Steel. In the study of axial stress and strain, it is typical to study a curve of axial stress σ
vs. axial strain ε
. The reasons for this are that such a curve captures important theoretical considerations and is also straight forward to generate experimentally (as was done in Lab #2). By analogy, a plot of shear stress τ
vs. shear strain γ
would reveal properties of shear, such as the shear modulus G
. However, in this lab, the specimen is a solid circular shaft. When this specimen is tested, the data that are collected are the torque T
supported by the shaft and the angle of twist ϕ
. The shear stress τ
and the shear strain γ
are not directly recorded. If the shaft is subjected to a small enough torque such that the entire shaft is within the linear elastic range, then we can easily deduce the shear stress and shear strain by the following relations: L
and J
T
, where ρ
is the distance away from the center of the shaft, J
is the polar moment of inertia of the cross section, and L
is the length of the shaft. If the shaft is loaded beyond the yield point (note that material at the outer edge of the cross section will yield first, and then interior portions will successively yield), then we must refer to the more general relations: L
tan
and
sec
x
dA
T
. Under the assumption that the shear stress is a function of the shear strain, that is )
(
ˆ
, it is possible to collect the T– ϕ
data and deduce points on the τ–
γ
curve without making any specific constitutive assumptions about the relation between shear stress and shear strain (this assumes that the specimen does not suffer any localized deformation, such as necking or cracking). However, this level of generality requires advanced mathematical reasoning that is beyond our scope. In practice, for many ductile materials, it is common to assume that the yield point occurs approximately at the proportional limit, and that beyond the yield point the shear stress is approximately constant, i.e.
τ
= τ
Y.
As the shaft is twisted, a point will be reached at which the material at the outer edge of the cross section will yield, but material on the interior is still below yield (Figure 1.a). As the shaft twisted beyond this initial yield, interior portions of the shaft will progressively yield. Note that even though the shear
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CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 26 of 36 stress is assumed to be constant, the torque T increases because the yielding material elements carry a higher stress (Figure 1.b). If the shaft is twisted sufficiently such that material over the entire cross section has yielded (Figure 1.c), the torque T
P
carried by the shaft at this point is the theoretical maximum torque that the shaft can carry (because no further increases of stress on the material are possible), and it can be shown that J
c
T
P
Y
4
3
. After this point has been reached, the T– ϕ
curve will be flat. Figure 1. Progressive Elastic-Plastic Shear Stress. Adapted from web.umr.edu/~be120/lessons/torsion/manual/ A.
Terminology Figure 2. Torque vs Twist per unit length Proportional Limit:
Farthest point to which proportionality of Torque vs. Twist per Unit Length extends.
Torque (T)
PL
Torque vs. Twist Per Unit Length (1020 Hot Rolled Steel) Twist Per Unit Length (Radians/L) Proportional Limit Ultimate Torque Linear elastic region
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CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 27 of 36 Elastic Limit:
Point beyond which the material will not return to its original length when unloaded. Modulus Of Resilience:
Area under shear stress vs. shear strain curve up to the proportional limit. It represents the energy that can be absorbed per unit volume without creating a permanent distortion. It is also equal to the area under the linear portion of the Torque vs. Twist per Unit Length curve divided by the cross sectional area of the shaft. Modulus of Rupture: Amount of energy required to cause rupture or fracture of specimen. It is equal to the area under the entire shear stress vs. strain curve. It is also equal to the entire area under the Torque vs. Twist per Unit Length curve divided by the cross sectional area of the shaft. II.
Laboratory Procedure Sample Material 1020 Hot Rolled Steel Testing Machine Tinius Olsen Torsion Machine Capacity 10,000 in-lb Measuring Device Troptometer and Graduated Chuck Gage Length 6”
troptometer
& 12”
graduated chuck Mount the 1020 steel shaft (Figure 3) between the grips in the Tinius Olsen Torsion Machine (Figure 4). Increasing magnitude of angle of twist is applied to the specimen and the corresponding values of the torques (T) in a gage length (L) of the specimen are recorded. The torque is measured directly off the Tinius Olsen Torsion Machine. The readout of torque is in in-lb. There are two gage lengths of 6” and 12”. Readings are recorded over a fixed gage length of 6” when the troptometer is mounted onto the steel shaft. The troptometer (Figure 5) is a device that accurately measures the angle of twist over a fixed gage length of 6”. Apply torque to the shaft and record the torque every 0.2
twist of the shaft using the troptometer. The troptometer will only be used until the material reaches yielding stage. Then the troptometer will be removed and further angular distortion measurements will be obtained from graduated degree markings on the moving chuck. At this time the gage length where the angle of twist is measured is 12”. Using the graduated degree marking, record the torque every 20
twist of the shaft up to 180
. Then proceed taking readings every 180
of twist until the shaft fractures. Record the angle of twist and the torque at fracture. Figure 3. Standard Dimensions of Steel Sample Used in Torsion Test 6” Gage Length Troptometer 0.75” 1 ” 12 “ 3 ” 3 ”
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CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 28 of 36 Figure 4. Tinius Olsen Torsion Machine Figure 5. Troptometer III.
Recorded Data Torsion Test of 1020 Hot rolled Steel Gage Length of Tropometer:
Gage Length of Graduated Chuck:
1 (recorded) 2 (recorded) 3 (calculated) 4 (calculated) Torque Twist Twist Increment Unit Twist
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CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 29 of 36 IV.
Results and Calculations 1.
Make two plots of the Torque (in-lb) vs. Unit Twist (rad/inch) data. One plot should show just the linear elastic region and the other should show all data up to the rupture. In order to find the Unit Twist, you must first convert the angle of twist (
) in degrees to radians. Once you have found the Twist in radians you must divide by the appropriate Gage Length. Twist (radians)
Unit Twist
Gage Length
2.
a.
Calculate the Shearing Stress at the Proportional Limit (
PL
) PL
PL
T
c
J
Where T
PL
= Torque at the proportional limit, c
= Radius of the shaft = 0.375”, and J = Polar Moment of Inertia = 0.5
c
4
b.
Assuming that the shear yield stress
Y
=
PL
, compute the ratio of the shear yield stress to the tensile yield stress (look up an accepted value). 3.
a.
Calculate the Shear Modulus G. Use the following relation to derive an expression for G, and state how your result can be interpreted in your graphs generated in question #1. TL
JG
for {0
T
T
y
and 0
y
} b.
A theoretical expression relating the shear modulus and Young’s Modulus is )
1
(
2
E
G
where ν
is Poisson’s Ratio. Compute G
from this formula and compute the %deviation away from your value in part a. 4.
Calculate the Modulus of Resilience (
M
res
).
This is the area under the Torque-Twist per Unit Length curve up to the proportional limit, divided by the cross sectional area of the shaft. 5.
Calculate the Modulus of Rupture. This is the area under the entire Torque-Twist per Unit Length curve, divided by the cross sectional area of the shaft.
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CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 30 of 36 6.
a.
Define T
PR
as the torque at the proportional limit. Define T
P
as the plastic torque, which is the torque carried by the shaft at rupture. Using the following formula from plastic theory, determine a relationship between T
PR
and T
P
. 3
4
P
Y
T c
J
b.
Using your result from a, compare the the theoretical value for T
P
with the result from the data observed in the lab, and compute the % deviation. V.
Conclusions Write a concluding statement according to the lab format guidelines. VI.
References
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CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 31 of 36 LAB #5: FLEXURE OF BEAMS I.
Objective and Background The objective of this lab is to show that the development of the fundamental beam theory for pure bending is substantially correct. This theory states that the axial strain and axial stress distributions are linear through the depth of beam. In particular, the axial strain at the neutral axis is zero, and the stress at a general location can be calculated using the equation: 𝜎
௫
=
−𝑀𝑦
𝐼
A.
Terminology Neutral Surface (N.S.):
The
surface of the beam through which the axial stress and strain are zero. The neutral surface passes through the centroid of the cross section and is sometimes called the centroidal surface. The coordinate axis that passes through the centroid of each cross section is called the centroidal axis, or neutral axis. II.
Laboratory Procedure Testing
:
The test specimen is an aluminum I-beam with the section dimensions shown in Figure 1. It is supported at its ends on rollers and loaded at the third points to produce a region of pure constant bending over the middle third. Such and experimental setup is called the Four-point Beam Loading (Figure 3). Electric resistance strain gages are mounted in the mid-span of the beam at the locations shown in Figure 2. The strain gages are used to measure the strain at various depths when the load is applied vertically downward using the Instron Testing Machine. Record the strain readings at each gage location, at each load level. Sample Material Aluminum I - Beam Testing Machine INSTRON 3369 Capacity 11K Measuring Devices Strain Indicators and Load Cell
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CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 32 of 36 III.
Recorded Data Load P
1 = _______________lb.
P
2 = _______________lb. Gage Number Strain Experimental Stress Strain Experimental Stress 1 2 3 4 5 Record data in the strain columns and calculate the stress columns based on the recorded strain.
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CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 33 of 36 IV.
Questions 1.
. Reproduce a copy of the data that was collected. Then make a separate table, as outlined below, to compare Experimental Stress with the Theoretical Stress, for both cases, P1 and P2. You should average your data for gages 1-2, and average your data for gages 4-5, as indicated below. The theoretical stress at any location can be calculated using the equation: 𝜎
௫
=
−𝑀𝑦
𝐼
To calculate experimental stress, use one dimensional Hooke's Law 𝜎 = 𝐸
ɛ
Note that the strain at each location is already measured, and 𝐸
is given. The moment of inertia about the z axis has to be determined as well. In order to calculate the theoretical stress, you must know the bending moment carried by a cross section of the beam. To find the maximum moment, draw shear and moment diagrams for the sample. By examining the diagrams, you can determine that the maximum bending moment in the beam is 𝑀 = (𝑃/2) ⨯ 4
. 2.
(a) Plot the experimental Stress vs. Depth in the beam for both the 𝑃
ଵ
and 𝑃
ଶ
.
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CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 34 of 36 (b) Draw a 3D sketch of the experimental stress distribution at the mid-span of the beam. Clearly indicate which regions are in tension and which are in compression. Is there any shear on this section (in theory). 3.
According to the theory of pure bending, the FBD of the left half of the beam looks something like the following: The net force and net moment about the centroid, point O, carried by the cross section can be calculated using the following integrals, where A is the portion of the cross section that is being considered. ∑ 𝐹
௫
= ∫
𝜎𝑑𝐴
∑ 𝑀
/
= − ∫
𝑦𝜎𝑑𝐴
Each integral can be calculated by dividing the entire cross section into smaller subsections, integrating over each subsection separately, and then adding the results. If the subsections are chosen carefully - as suggested by the figure on the next page - then each integral can be calculated by a (stress)(area) or (stress)(area)(distance). (a)
Referring to the explanations and diagram below, complete the following table twice, once for 𝑃
ଵ
and once for 𝑃
ଶ
:
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CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 35 of 36 -
𝛔 − 𝐚𝐯𝐠
average stress acting on portion of cross section corresponding to given location [
𝛔 − 𝐚𝐯𝐠 = (𝛔
௧
+ 𝛔
௧
)/2]
-
width
... width of portion of cross section corresponding to given location (positive) -
height
... height of portion of cross section corresponding to given location (positive) -
R
... resultant force on portion of cross section corresponding to given location (positive or negative, measured with x-axis as positive) -
y-centroid
. vertical coordinate of the centroid of the portion of cross section corresponding to given location, measured from the neutral axis (can be positive or negative) -
M
... net moment about the centroid due to the forces that act on the portion of the cross section corresponding to given location (should turn out to be positive) (b) Does your data verify horizontal force equilibrium for the FBD of the left half of the beam?
𝐹
௫
= න
𝜎𝑑𝐴
= 0?
(c)
Does your data verify the moment balance about the neutral surface of the left half of the beam
?
𝑀
/
= − න 𝑦𝜎𝑑𝐴
=
𝑃
2
𝐿
3
=
𝑃𝐿
6
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CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 36 of 36 APPENDIX A I.
Factorial Design of Experiments Factorial Design is a method for designing experiments in which all possible combinations of factors and all their levels are tested. A “3 x 4 factorial design” is an experiment with 2 factors, one of with has 3 levels, and the other has 4. Testing all possible combinations of factors and levels would require 3 x 4 = 12 separate experimental runs. A.
Response The response is the measured outcome of an experiment, the dependent variable or variables. In Lab 1, the Design of Concrete Mixture, the response is compressive strength. B.
Factors Factors are the parameters that can be modified, the independent variables, for each experiment. In Lab 1, the Design of Concrete Mixture, the factors are the ratio of water to cement and the age of the concrete. C.
Levels Levels are the discrete values, qualitative or quantitative, that a factor may have. In the case of quantitative levels, the response is assumed to be linear. Any other type of response, such as quadratic, requires some other type of experimental design. In Lab 1, the Design of Concrete Mixture, the two levels are the ratio of water to cement and the age of the concrete, and both of them are quantitative. D.
Null Outcome A null outcome is the case in which none of the combinations of factor levels have an effect on the response. E.
Main Effects A main effect is a response that is a consistent difference between levels of a factor. In Lab 1, the Design of Concrete Mixture, if the compressive strength of the concrete is found to vary with the ratio of water to cement no mater what the age of the concrete, then the ratio of water to cement is a main effect. F.
Interaction Effects An interaction effect is a response in which the difference due to one factor depends on the level of another factor. In Lab 1, the Design of Concrete Mixture, if the compressive strength of the concrete is found to vary with the ratio of water to cement when the
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CivEng Introduction to Solid Mechanics UWM 203 Lab Manual 2022 Page 37 of 36 concrete is young but not when the concrete is old, then there is an interaction between the two factors. II.
2
k
Factorial Design of Experiments A specific instance of Factorial Design is 2
k
Factorial Design in which each factor only has two levels. The number of separate experimental runs necessary to test all possible combinations of factors and levels is 2
k
, where k
is the number of factors. By convention, when there are only two factors, they are labeled “A” and “B”. III.
2
2
Factorial Design of Experiments A specific instance of 2
k
Factorial Design is 2
2
Factorial Design in which there are only two factors, and they both have only two levels. The number of separate experimental runs necessary to test all possible combinations of factors and levels is 2
2
= 4. By convention, when there are only two levels, they are labeled “–“ or “low” and “+” or “high”. IV.
Statistical Analysis V.
Conclusions VI.
References Douglas C. Montgomery, Engineering Statistics
, 4th Edition, John Wiley & Sons. “Research Methods Knowledge Base”, William M.K. Trochim, 2006, www.socialresearchmethods.net/kb/expfact.php Wikipedia, en.wikipedia.org/wiki/Factorial_experiment
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