Part A.
Introduction
Brief introduction on SMA materials. This information may also be presented on the CRCD website.
The SMA Tube is held in place by a torsion
test frame. The frame is designed to
where a specimen is constrained at one end where there is a Transducer
Techniques TRT-500 Torque cell. The other end of the specimen is free to
rotate. The rotation is measured by a rotational potentiometer near the free
end. The specimen is heated by heating elements placed around the tube.
Thermocouples are arrayed over the inner and outer surface of the tube in order
to measure the temperature at these locations. Temperature, load, and rotation
values are collected from the experiment approximately once a second.
The computer uses the temperatures to establish a temperature profile throughout the specimen and to help control the heating elements. The temperatures at multiple locations are collected and analyzed to calculate the average temperature at five evenly distributed points along the length of the specimen.
The load applied to the tube is measurered through the load cell. The strain of the specimen is measure red using the potentiometer (a variable resistor with a rotating slider). The control program for this experiment then calculates the stress ands strain the tube experiences. These values and the various temperatures are output to the data file torsiondata.txt for later analysis.
J=(p/32)*(Do4- Di4)
Twist (Rotation) ______________
Shear Strain ______________
Shear Stress ______________
Now the same tube has been cooled to 20 degrees Celsius where it is in its martensite phase. Calculate the twist at x = 5 cm. Calculate the shear strain for the SMA tube. Calculate the max shear stress.
Twist (Rotation) ______________
Shear Strain ______________
Shear Stress ______________
Sketch Strain vs. Temperature for both the austenite and the martensite phases of the material.
Write the steps necessary for the students to begin the experiment. Have students open computer data file and the computer data acquisition program.
Part D.
Development of SMA Strain Equation
Part E.
Conclusions
|
Material
Property |
Austenite |
Martensite |
|
Thermal
conductivity coefficient |
0.18 W/cm * deg C |
0.086
W/cm * deg C |
|
Young’s
Modulus* |
83 GPa |
35 GPa |
|
Poisson’s
Ratio |
0.33 |
0.33 |
|
Coefficient
of Thermal Expansion |
11.0E-6/deg.
C |
6.6E-6/deg.
C |
|
Density |
6.45
g/cu.cm |
6.45
g/cu.cm |
|
Shear
Modulus |
29 GPa |
11 GPa |
* Highly nonlinear with temperature (this will be ignored for this assignment)