CE 311 Lab Report 1 L Mauriot
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CE 311 – CIVIL ENGINEERING MATERIALS LABORATORY
Section Number:
L-M01
Experiment Number:
1
Experiment: Stress-Strain Relationships from Tension Tests
Submitted by:
Louis Mauriot
Submitted to:
Soroush Mousavinezhad
Date Experiment Performed:
08/28/23
Date Experiment Report Submitted: 09/07/23
Name of People Who Participated:
Louis Mauriot
Leah Clark
Juan Limas
Sonya Shanbhag
Table of Contents
ABSTRACT
................................................................................................................................................
3
PROBLEM STATEMENT
............................................................................................................................
3
EXPERIMENTAL METHOD
........................................................................................................................
3
RESULTS
...................................................................................................................................................
3
Graph 1: 1045 Hot Rolled
....................................................................................................................
4
Graph 2: 1045 Hot Rolled Enhanced
....................................................................................................
4
Table 1: Reported Numerical Data for 1045 Hot Rolled
......................................................................
4
Graph 3: 1045 Cold Rolled
...................................................................................................................
4
Graph 4: 1045 Cold Rolled Enhanced
..................................................................................................
4
Table 2: Reported Numerical Data for 1045 Cold Formed
...................................................................
4
Graph 5: Brass
.....................................................................................................................................
5
Graph 6: Brass Enhanced
.....................................................................................................................
5
Table 3: Reported Numerical Data for Brass
........................................................................................
5
Graph 7: Copper
..................................................................................................................................
5
Graph 8: Copper Enhanced
..................................................................................................................
5
Table 4: Reported Numerical Data for Copper
....................................................................................
5
Graph 9: Aluminum
.............................................................................................................................
6
Graph 10: Aluminum Enhanced
...........................................................................................................
6
Table 5: Reported Numerical Data for Aluminum
................................................................................
6
Graph 11: Cast Iron
..............................................................................................................................
6
Graph 12: Cast Iron Enhanced
.............................................................................................................
6
Table 6: Reported Numerical Data for Cast Iron
..................................................................................
6
Picture of Each Sample After Fracture
.................................................................................................
7
CONCLUSIONS
.........................................................................................................................................
7
APPENDIX A
.............................................................................................................................................
7
Table: Specimen Dimensions
...............................................................................................................
8
ABSTRACT
This initial laboratory experiment allowed us to study and obtain detailed information about the different stress strain relationships for steel and aluminum coupon samples. 6 specimens of steel and aluminum were subjected to a load and elongated until the fracture point was reached. Using the data obtained, stress strain graphs were plotted on Excel for each specimen and calculations were performed. Each specimen was compared and discussed. PROBLEM STATEMENT
The determination of the stress-strain relationships while performing tension tests on coupon samples for steel and aluminum and studying the resulting data through calculations and graphical plotting were the objectives of this laboratory experiment. The resulting comparison between the different specimens, understanding the different stress strain relationships to be able to better categorize them for different uses in structural/construction purposes of civil engineering also was among the objectives of this experiment.
EXPERIMENTAL METHOD
A total of 6 specimens were subjected to a tension test (1045 Hot Rolled Steel, 1045 Cold Finish Steel, Copper, Brass and Cast Iron). Each specimen consequently experienced an elongation of the gage while a load was applied to each one until the complete fracture point. Using the elongation data recorded on the computer during the performing of each test, and the load data, we then calculated and
plotted the strain vs strain corresponding graphs. Afterwards, we studied the graphs in detail by finding the corresponding proportional limit, the offset, ultimate stress and the strain at that corresponding point and the fracture stress and strain if specimen is fractured. Calculations were performed to obtain the ductility, the strain hardening ratio and the modulus of elasticity. Finally, the type of failure and yield
behaviors, the effects of carbon content, and the shape of the stress strain curve compared with each specimen was discussed.
RESULTS
Initially, we have each stress strain graph for each specimen tested from 1045 Hot Rolled to Cast Iron presented with the enhanced graphical result focusing on the elastic part of the curve for each.
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Related Questions
7:50
ul LTE O
A docs.google.com
Choose the correct answer *
During the tensile test, experiment on a sample of mild steel, data represented in the
figure below was obtained with an initial diameter (do) of 0.505 inch. At failure, the
reduced diameter (d) of the sample was 0.305 inch. Gauge Length (Lo) is 2 inches
and final Gauge Length (L,) is 2.625 inches. Answer the questions below:
Us
70
Tk
LyP
IR
50-
FL
PL ptiel linit
AL or 6T
P
EL lastie lii
UP per yied paint
Lypi Lewer s
us t uni mated streagth
IR: Indicatul siregh
Rupture
TR True strugth Ruple
fPL (propartimal timt)
Direct strain
& to
to
E strmin Cin/in)
a
b
1. Mild steel
is: (a) brittle
materials (b)
ductile
material (c)
between the
ductile and
the brittle
2. Young's
Modulus
evaluates
elasticity
within the
region from:
(а) 0 -
Proportional
Limit. (b)
Proportional
Limit - Lower
yield Point.
(c) Lower
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Calculate the tensile stress when applied force of 120OON on specimen of
* diameter of 7mm
111 O
211 O
311 O
411 O
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A steel specimen of 300 mm length and 30 mm diameter is subjected to tensile test in a computerizedUTM. Under 54 kN of tensile load, the final length and diameter are observed as 300.112 mm and29.99634 mm respectively. Calculate (a) the Poission’s ratio and (b) the values of three moduli.
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an
30
Show Transcribed Text
The varying, fluctuating stresses
shown to the below are found at
the critical location of a
component. The material is
steel, the fully adjusted
endurance limit is 25 ksi, the
ultimate strength is 200ksi. The
fatigue strength fraction is f =
0.77.
What is the life of the part in
hours if this 6 second stress
pattern continues to repeat for
the remainder of the part's life?
Show Transcribed Text
Less than one hour
10 to 20 hours
39 to 42 hours
43 to 45 hours
50 to 55 hours
100 to 105 hours
t(sec)
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The following data were obtained from the tensile test of Aluminum alloy. The initial diameter of testspecimen was 0.505 inch and gauge length was 2.0 inch. Plot the stress strain diagram and determine(a) Proportional Limit (b) Modulus of Elasticity (c) Yield Stress at 0.2% offset (d) Ultimate Stress and(e) Nominal Rupture Stress.
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b) If the original sample length prior to testing was 63 mm, what is the maximum length that it
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c) What is the difference between elastic strain and total strain?
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B
A
B
C
Load (kgf)
4800
8400
7200
Elongation (mm)
0.192
28.8
38.4
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- 7:50 ul LTE O A docs.google.com Choose the correct answer * During the tensile test, experiment on a sample of mild steel, data represented in the figure below was obtained with an initial diameter (do) of 0.505 inch. At failure, the reduced diameter (d) of the sample was 0.305 inch. Gauge Length (Lo) is 2 inches and final Gauge Length (L,) is 2.625 inches. Answer the questions below: Us 70 Tk LyP IR 50- FL PL ptiel linit AL or 6T P EL lastie lii UP per yied paint Lypi Lewer s us t uni mated streagth IR: Indicatul siregh Rupture TR True strugth Ruple fPL (propartimal timt) Direct strain & to to E strmin Cin/in) a b 1. Mild steel is: (a) brittle materials (b) ductile material (c) between the ductile and the brittle 2. Young's Modulus evaluates elasticity within the region from: (а) 0 - Proportional Limit. (b) Proportional Limit - Lower yield Point. (c) Lowerarrow_forwardCalculate 6 Calculate the tensile stress when applied force of 120OON on specimen of * diameter of 7mm 111 O 211 O 311 O 411 Oarrow_forwardProblem 24.16 It has been observed that the yield strength of the material of a component is normally distributed with a mean of 230 N/mm² and a standard deviation of 30 N/mm². The stress induced in the component is also normally distributed with a mean of 150 N/mm² and a standard deviation of 15 N/mm². Determine the reliability used in designing the component.arrow_forward
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