Experiment-7
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University of Central Oklahoma *
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2143
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English
Date
Dec 6, 2023
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Pages
7
Uploaded by HighnessScorpionMaster539
University of Central Oklahoma
Experiment 7 - Beam Experiment
Dylan Robinson, Joshua Jackson, and Kaleb Paddock
Dr. Adnan Al-Ibadi
Thursday 1:00 PM
11/10/22
ABSTRACT
In experiment 7 for the strength of materials lab, we employ the use of strain gauge
system in order to determine the static deformation of a cantilever beam structure, as well as
learn some of the basics involving the basics of finite element analysis.
[1]
In aerospace engineering, aircraft wings’ lateral structural elements are similar to that of
bridge beams. They are referred to as spars and they carry the main loadings induced from lift.
Figure 1 shows equations related to spar shear force and bending moment.
Figure 1. Aircraft Wing Spar
THEORY
For this experiment,we are asked to consider the deformation of a cantilever beam
structure using the theories and concepts behind finite element analysis in conjunction with a
strain gauge system. For our particular experiment, we use the strain gage system on a
cantilever beam and gather experimental data from that.
EQUIPMENT
As stated previously, the main piece of equipment that we will be using in this particular
experiment is a strain gauge system. This tool is particularly useful when trying to determine
deformation on a body, and in this particular experiment in which we are testing on a simple
apparatus, it is relatively lightweight work on the end of this device.
This device’s main components consist of a single conducting strip on a film that “zig
-
zags”
back and forth along the longitudinal axis of the beam. The gauges are able to detect
strain in the beam in that direction, and thus will be able to give us very accurate measurements
for the total deformation on the specimen.
Shown below is a diagram of the circuit that is used for the strain gauge. Figure 3 shows
the exact components used.
Figure 2. Strain Gage Diagram
EXPERIMENTAL METHOD
In this experiment, our part of setting up the experiment was very limited. However, as
stated previously, our particular experiment involved a cantilever beam setup with an
attachment point for an added load point (weight) towards the end of the beam, and given
various loads applied, we measured the deformation of the specimen from the strain gauge
system. Shown below in Figure 3 is the apparatus setup.
[3]
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