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CEE 370 Mechanics of Materials Lab
BEAM BENDING THEORY
He Shi
University of Hawaii at Manoa
CEE 370L Mechanics of Materials
Nov 26, 2023
1
CEE 370L Mechanics of Materials
Laboratory 1
Fall 2023
EXECUTIVE SUMMARY
During an experiment, an aluminum beam was examined to validate the principles of
beam bending. The theory suggests that a beam made of flexible & homogeneous material with
an equivalent modulus of elasticity in tension and compression will deform equally under the
same stress. The moment of inertia (I) was calculated for bending around the horizontal centroid
axis using the provided properties of the beam section. The moment about the maximum load at
the plane section was determined using a shear force and bending moment diagram. Stresses
were computed using the moment of inertia, moment about the plane surface, and distance from
the centroid axis. It was proven that the distributed loads on the top and bottom flanges were
very close to each other, thus confirming the theory.
During the beam experiment, loads were applied which caused sagging. As a result,
throughout the beam, there was a positive bending moment. Gauges on the plane section of the
beam indicated that a plane section within the beam before bending remains plane after bending
throughout a constant moment section of the beam. This proves that the beam bending theory is
accurate. The experiment concluded that the material is linearly elastic, as the relationships
between stress and strain were directly proportional. When a load was applied, the top of the
beam was in compression while the bottom of the beam was in tension. The lowest sagging point
of the beam showed the largest strains, and therefore had the largest stresses.
CEE 370L Mechanics of Materials
Laboratory 1
Fall 2023
1 Introduction
1.1 Background
A transverse load is applied to an aluminum beam in order to test the beam bending
theory. A number of electrical resistance strain gauges are attached at various points on the
beam to measure strain. The purpose of the testing is to confirm the relationship between
moment and bending stresses.
1.2 Reason for Experiment
The purpose of this lab was to test the deflection limits of beams that are installed in
buildings. The experiment provided valuable information to engineers regarding how beams
support and resist loads, which enables them to ensure the safety and stability of structures.
Finding the maximum values of quantities and their locations along the beam is essential for
beam design.
1.3 Theory
When a beam is subjected to loads that are transverse to its length, there is no axial load
applied. However, when a transverse load is applied, a relationship can be found between the
bending moment and the transverse deflection of the beam. The beam is made of a linearly
elastic material, which means it follows Hooke's Law. Therefore, a small deflection should cause
small angles due to the deflection.
The moment-curvature equation ( is determined by the bending moment divided by
the modulus of elasticity times the moment of inertia (also known as the flexural rigidity).
The equation given for the moment-curvature is:
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CEE 370L Mechanics of Materials
Laboratory 1
Fall 2023
where M is the bending moment and EI is the flexural rigidity.
The flexure formula ( is determined by the bending moment multiplied by the distance from
the neutral distance divided by the inertia of the cross section. The equation given for the flexure
formula is:
where M is the bending moment, y is the distance from the neutral axis, and I is the moment of inertia of
the cross section
1.4 Objective
The goal of this laboratory experiment was to confirm the correlation between bending
moments and bending stresses and assess whether the stress distribution aligns with the
principles of beam bending theory.
CEE 370L Mechanics of Materials
Laboratory 1
Fall 2023
2 Approach
2.1 Test Setup and Instrumentation
The experiment was done with a load cell. There were a total of 20 strains on the steel,
five on the back, front, top, and bottom. Each of the strains were 6 inches apart from each other.
The strains are then hooked up to three different boxes. The load cell co impressed the aluminum
beam at 0 kips to 2 kips in 1 increment and back down to 0 kips
CEE 370L Mechanics of Materials
Laboratory 1
Fall 2023
2.2 Test Specimens
Material
Length
(inches)
Length
Between
Load
Points
(inches)
Tube Steel
96.00
48.00
2.3 Test Procedure
• Load applied to specimen: total transverse load - 0, 1, 2, 1, 0 kips
• At each load level, record the microstrain reading from each gage
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CEE 370L Mechanics of Materials
Laboratory 1
Fall 2023
The moment of inertia, span length, and length between load points of the tube steel were
measured and recorded. Then, the measurements were placed in the frame of the
RIEHLE machine. After that, 20 different electrical resistance strains were applied to
the front, back, top, and bottom of the object. The data was collected from the steel
specimen at 0 kips, 20 times for each strain. Later, a force of 1 kip was loaded and 20
measurements were recorded from each side. Finally, the entire process was repeated
three more times for forces of 2 kips, 1 kip, and 0 kips.
3 Results
3.1 Overview
Table 3-1.1: Measured Strains
Load(kips)
Strain(ksi)
T1
T2
T3
T4
T5
0
-0.000003
-0.000002
-0.000002
-0.000002
0
1
0.000088
0.00009
0.00009
0.000083
0.000068
2
0.000182
0.000182
0.000184
0.000168
0.000139
1
0.00009
0.000093
0.000092
0.000084
0.000071
0
-0.000005
-0.000002
-0.000003
-0.000003
0.000002
U1
U2
U3
U4
U5
0
0
0
0
0
-0.000004
1
-0.000089
-0.000088
-0.000089
-0.000074
-0.000068
2
-0.000175
-0.000172
-0.00017
-0.000148
-0.000131
1
-0.000094
-0.00009
-0.000083
-0.000074
-0.000068
0
-0.000005
0
0.000011
0.000003
0
F1
F2
F3
F4
F5
0
-0.000005
-0.000003
-0.000003
-0.000003
0
CEE 370L Mechanics of Materials
Laboratory 1
Fall 2023
1
0.00006
0.000031
0
-0.000032
-0.00006
2
0.000119
0.000059
-0.000003
-0.000064
-0.000121
1
0.000058
0.000028
-0.000005
-0.000036
-0.000065
0
-0.000006
-0.000006
-0.000004
-0.000005
-0.000003
B1
B2
B3
B4
B5
0
-0.000004
-0.000002
0
-0.000005
-0.000001
1
0.000057
0.000029
-0.000003
-0.000036
-0.000062
2
0.000119
0.000061
-0.000001
-0.000065
-0.000119
1
0.000059
0.00003
-0.000003
-0.000038
-0.000065
0
-0.000006
-0.000004
-0.000003
-0.000006
-0.000003
Table 3-1.2: Measured Stress
Load(kips)
Stress(ksi)
T1
T2
T3
T4
T5
0
-0.087
-0.058
-0.058
-0.058
0.000
1
2.552
2.610
2.610
2.407
1.972
2
5.278
5.278
5.336
4.872
4.031
1
2.610
2.697
2.668
2.436
2.059
0
-0.145
-0.058
-0.087
-0.087
0.058
U1
U2
U3
U4
U5
0
0.000
0.000
0.000
0.000
-0.116
1
-2.581
-2.552
-2.581
-2.146
-1.972
2
-5.075
-4.988
-4.930
-4.292
-3.799
1
-2.726
-2.610
-2.407
-2.146
-1.972
0
-0.145
0.000
0.319
0.087
0.000
F1
F2
F3
F4
F5
0
-0.145
-0.087
-0.087
-0.087
0.000
CEE 370L Mechanics of Materials
Laboratory 1
Fall 2023
1
1.740
0.899
0.000
-0.928
-1.740
2
3.451
1.711
-0.087
-1.856
-3.509
1
1.682
0.812
-0.145
-1.044
-1.885
0
-0.174
-0.174
-0.116
-0.145
-0.087
B1
B2
B3
B4
B5
0
-0.116
-0.058
0.000
-0.145
-0.029
1
1.653
0.841
-0.087
-1.044
-1.798
2
3.451
1.769
-0.029
-1.885
-3.451
1
1.711
0.870
-0.087
-1.102
-1.885
0
-0.174
-0.116
-0.087
-0.174
-0.087
Figure 3-1.1 stresses in the top and bottom gages at mid-span for each load level
Figure 3-1.1 Stresses of the Top and Bottom Strain Gages
In Figure 3-1.1, the graph depicts the relationship between the load at each level and the
stresses on the top and bottom. The blue line in the graph represents the top stress data, while the
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CEE 370L Mechanics of Materials
Laboratory 1
Fall 2023
red line represents the bottom stress data. It's important to note that the graph only pertains to the
mid-span portion, specifically T1 and U1.
Figure 3-1.2: Average Stresses of the Front and Back Strains
Figure 3-1.2 shows the relationship of the distance from the neutral axis to the average
stresses of the front and back strains. The graph only shows the data collected from the 2 kips
load. The graph also shows the stresses from T1 and U1.
CEE 370L Mechanics of Materials
Laboratory 1
Fall 2023
Figure 3-1.3: Top and Bottom Stresses from Mid-Span to Support
In Figure 3-1.3, we can see how the top and bottom stresses vary in relation to the distance
from mid-span to the support. The blue line represents the data collected for the top stress while
the red line represents the data collected for the bottom stress.
4 Analysis
4.1 Tube Steel Specimen Analysis
Based on the data collected during the experiment, it was found that the force with the highest
load (2 kips) resulted in the most strain. The strain gages located at the top of the specimen
showed the largest strain, while those at the bottom showed the smallest. Moreover, the front and
back strain gages displayed a deviation of the data going from positive to negative.
CEE 370L Mechanics of Materials
Laboratory 1
Fall 2023
In Figure 3-1.1, there are two linear lines in blue and red colors. The blue line represents the top
stresses and moves towards the positive direction, while the red line represents the bottom
stresses and moves towards the negative direction. The theoretical stress would show two linear
lines originating from the origin and extending towards the positive or negative direction. Upon
comparing the measured stress with the theoretical stress, we observe that both the top and
bottom measured stresses align with the theoretical stress. However, upon closer inspection of
the red line, we can see a gap indicating that the data collected from the bottom strain was larger
when reverting to 2 kips to 1 kip than the first time we recorded the bottom data.
The graph in Figure 3-1.2 represents the average stress of the front and back, which is shown by
a semi-straight line. The theoretical stress should be a straight line through the origin. Comparing
these two stresses, the measured stress shows a slight curve at the end, but the data was still able
to create a line.
In Figure 3-1.3, there are two lines going towards zero. The blue line indicates the top stresses
collected from the mid-span to the support, while the red line indicates the bottom stresses. The
theoretical stress will show a linear line in the first half and then begin to travel to zero.
Comparing the stresses, both the measured stresses align with the theoretical stress.
Based on what we learned in class, a plane will be perpendicular to the neutral axis of the
theoretical lines if they are correct. Based on the graphs shown, all theoretical lines almost or
perfectly line up with the measured lines. The stress distribution agrees with the beam bending
theory because the theory states that cross-sections of the beam must remain plane during
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CEE 370L Mechanics of Materials
Laboratory 1
Fall 2023
bending. The tube steel remained symmetric to the longitudinal axis during the experiment, and
there were not any significant errors in the results of the experiment.
5 Conclusions/Recommendations
Based on the data collected, the following conclusions can be made:
- The top strains had the highest number of strains, while the bottom strains showed the
smallest number of strains.
- Both strains data were observed when the load was at 2 kips.
- The front and back strain gauges showed both positive and negative data.
- All the graphs almost or perfectly aligned with the theoretical stress.
- As the steel beam remained unchanged after the experiment and the stresses aligned
with the theoretical, the stress distribution corroborates the beam bending theorem.
- No significant errors were discovered during the experiment.
- Plane sections remained plane in constant moment portions of the beam
From the experiment, recommendations for the lab would be to use a more accurate
loader and to use a beam that has not been in many previous experiments. This could lower the
margin of error in the lab.
CEE 370L Mechanics of Materials
Laboratory 1
Fall 2023
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Tensile strength
Tఅబండి
Specific weight
bai
MPa
10 psi
GPa
Iblin
Matrix materials:
Polyester
Ероху
Aluminum
10
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45
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27.1
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Filler materials:
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470
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3240
5650
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3450
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820
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500
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You are a biomedical engineer working for a small orthopaedic firm that fabricates rectangular shaped fracture
fixation plates from titanium alloy (model = "Ti Fix-It") materials. A recent clinical report documents some problems with the plates
implanted into fractured limbs. Specifically, some plates have become permanently bent while patients are in rehab and doing partial
weight bearing activities.
Your boss asks you to review the technical report that was generated by the previous test engineer (whose job you now have!) and used to
verify the design. The brief report states the following... "Ti Fix-It plates were manufactured from Ti-6Al-4V (grade 5) and machined into
solid 150 mm long beams with a 4 mm thick and 15 mm wide cross section. Each Ti Fix-It plate was loaded in equilibrium in a 4-point bending
test (set-up configuration is provided in drawing below), with an applied load of 1000N. The maximum stress in this set-up was less than the
yield stress for the…
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X Strength of Materials. (Midterm
x Desmos | Scientific Calculator
x My Questions | bartleby
x Calculus Calculator - Symbolab
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. الإشارات الأخری
H التطبيقات
مطلوب
Section
5
3 m
2m
2 m
The rigid beam ABC is supported by pin A and wires BD and CE. If the load P on the beam
causes the end C to be displaced 6 mm downward. What is the normal strain developed in
* ?wire BD
)2 نقطة(
0.0015 C
2.57 O
0.00107
10:02 PM
AR
11/29/2020
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Test Specimen
4140 CF steel
6061 T6 Al
Gray Cast iron 40
FC Brass 360
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48.5 ft-lb
25 ft-lb
12 ft-lb
27 ft-lb
Impact Strength (J/m
or ft-lb/in)
123.096 ft-lb/in
63.452 ft-lb/in
What is the final analysis/ overall observation from the data?
30.457 ft-lb/in
68.528 ft-lb/in
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I need an answer in half an hour
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Part A
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Express your answer with the appropriate units.
?
h =
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ISBN:9781259822674
Author:Yunus A. Cengel Dr., Michael A. Boles
Publisher:McGraw-Hill Education
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Control Systems Engineering
Mechanical Engineering
ISBN:9781118170519
Author:Norman S. Nise
Publisher:WILEY
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Mechanics of Materials (MindTap Course List)
Mechanical Engineering
ISBN:9781337093347
Author:Barry J. Goodno, James M. Gere
Publisher:Cengage Learning
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Engineering Mechanics: Statics
Mechanical Engineering
ISBN:9781118807330
Author:James L. Meriam, L. G. Kraige, J. N. Bolton
Publisher:WILEY