Airfoil Testing Facility

The goal of the project is to design a new test apparatus for airfoil analysis. We will create a program that will automate the zero angle of attack (AOA) and provide real time feed back of the lift, drag and moment forces on the airfoil.

=Problem Definition=

Value Proposition
Using the wind tunnel for airfoil testing at the University of Idaho is a tedious process when it comes to set up and testing. The stand that airfoils are mounted on is antiquated, angle of the foil must be adjusted manually, and the accuracy is not as precise as it could be. The HotWings team is creating an airfoil testing apparatus to fix these issues through automation. Using computer software to adjust the angle of attack as well as calculate lift, drag, and moment forces through data collection. Additionally, it will be easy to set up, break down, and store away for later use by one individual.

Wind Tunnel             and                   Old Testing Equipment



(Left)The inside area of the plexiglass test section is 18 inches by 18 inches.

(Right) This is a full view of the original airfoil stand. This stand used a compression load cell to analyze the lift and drag forces. By calibration, the potentiometer was able to determine the "zero" angle-of-attack's position by displaying the least lift and drag forces.

Old Data Acquisition Display





Objectives
Primary
 * Operate a stepper motor at 0.1° increments.
 * Design and manufacture airfoil.
 * Design and manufacture a modular stand with load cell placement as a primary consideration.

Secondary
 * Physically integrate load cell into the system.
 * Create a stand assembly process diagram for users.
 * Use load cell to achieve lift, drag, and zero angle of attack measurements.

=Final Designs=

Stand Designs


The figure on the left is the full assembly of the airfoil stand and indicating the direction of the air flow through the test section.

The figure on the right is a top angled view of the stand to show more details.

Load Cell Positioning


The load cell is located above the motor and will rotate when the motor rotates. This design desigion weas made in order to obtain load cell reading more directly. During operation, the motor gennerates an abundance of heat and that can disturb the reading of the load cell. One way to design out the heat affecting the data from the load cell was to position the load cell with some distance above the motor.



LabView Front Panel


The LavView interface (GUI) is user friendly. We have started with this simple concept to illustrate our vision for the final concept. This GUI allows us to continue to keep in sight of our goals for the project. The GUI will be programmed with all features working and will be able to receive information provided by the load cell. This is important to the 0° Angle of Attack function. We will be working towards having the background code receiving data from the load cell and then translate the information to tell the motor to turn clockwise(CW) or counterclockwise(CCW). Our goal is to have the "Start" button accomplish that entire task.

=Validation=

This is a link to all the tests that the Airfoil Test Facility Team completed to ensure our structure will perform the way it is intended.



=Team Members=

=Additional Documentation=

Project Schedule




 * Schedule will be updated periodically throughout the project.

Meeting Minutes



Instructor-Client Meeting Minutes



Presentations



Client Interview