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Activities may be standalone, or part of lessons or curricular units. TE Activity: Windy Tunnel
Learning Objectives (Return to Contents) After this activity students, should be able to:
Materials List (Return to Contents) Each group should have:
Introduction/Motivation (Return to Contents) If you arm wrestle someone, who wins? Well of course, the person who exerts the most force wins! But, if both "wrestlers" push with the same force, their arms do not move. Lift on airplane wings is somewhat similar. As air flows over the top and bottom of the wing the pressure and velocity of the air change. These changes create lift. But on a symmetric wing, the changes on the top half match the bottom half. If the forces on the top and bottom of the wing are the same, there is no lift. Because the cambered airfoil (the curve in the wing) is not symmetric, the forces on the top and bottom are different — in this case lift is generated. Can you ever have lift on a symmetric airfoil? Yes, if you raised the nose of the airplane. This would place the wing at an angle. Engineers call this the angle of attack. Now the forces on the top and bottom of the wing are different and will create lift. The greater the angle of attack, the more lift; however, this only works up to a certain angle. If the angle is too high, the air will not flow smoothly over the airfoil and no lift can be created; the wing will stall, which means it will lose lift. Engineers often use wind tunnels to see how the air is flowing and if it flows smoothly over a wing. They do this by filling a wind tunnel's air chamber with smoke and allowing that (smoky) air to blow over a model wing. This process also allows them to determine how much drag an airfoil has by the size of the wake (an area whose airflow is not smooth at the trailing edge of the airfoil). Finally, they can also see stall when the air has separated from the wing and actually starts to flow towards the front the airfoil. Now try out the virtual wind tunnel! Procedure (Return to Contents) Background on Wind Tunnels If you cut a wing from its leading (front) edge to its trailing edge (back), the "cutaway" illustrated in the Figure 1 is what you would see. Aeronautical engineers call this an airfoil.
The top and bottom halves of the first airfoil are identical — this is referred to as symmetric. The airfoil on the right is not symmetric: its top and bottom halves are different. The difference in the bottom from the top means this airfoil is cambered. The Four Forces of Flight The four forces of flight are lift, weight, thrust and drag. Lift and weight are opposites and will counteract one another. Likewise, thrust and drag will counteract one another. How Does the Bernoulli Principle Create Lift? The top of a plane's wing is longer than the bottom because it is curved (see Figure 2). This means air will travel faster over the top of the wing than under it. As a result, the air moving over the top has less time to push on the wing, creating less air pressure than air passing below the wing. In the diagram below, the air moving under the wing moves slower and exerts more pressure/force on the wing than does the air moving over the wing. Since there is more force under the wing than above it, the net result is that the wing rises up, creating lift. This principle forms the basis of winged flight.
There are flaps on the front and back edges of the wing. During takeoff and landing, pilots extend the flaps on the back edge of the wing. The flaps increase the curve of the wing, which maintain the lift at slower speeds. After takeoff, the pilot retracts (puts back in) the flaps. Engineers continuously test their designs of wings to determine the lift, and in so doing, they must consider the following when testing:
Before the Lesson
With the Students
Instructions for Virtual Wind Tunnel
Attachments (Return to Contents) Safety Issues (Return to Contents) There are no safety issues since this is a computer activity. Troubleshooting Tips (Return to Contents) Make sure students understand the directions. Make sure all computers are preset to the appropriate website. Be sure to have students read the background information or go over it as a class. Assessment (Return to Contents) Pre-Activity Assessment Discussion Question/Answer: Ask students questions and have them raise their hands to respond. Write answers on the board
Activity Embedded Assessment Worksheet: Have the students record observations and comments on their Windy Tunnel worksheet. After students have finished their worksheet, have them compare answers with their peers. Discuss as a class. Post-Activity Assessment Figure drawing/Race: Draw an airfoil on the board (see Figure 1 for sample airfoils). Have two students come to the board and race who can draw (with chalk or whiteboard marker) the top or the bottom of the airfoil the fastest. The student who "wins" completes the drawing (gets to the end of the airfoil) first. Which student was the fastest? Will that airfoil create lift or not? Activity Extensions (Return to Contents) A great teacher demo on lift is to throw a Frisbee. The shape of the top of the Frisbee is smooth and air flows over the top faster, creating less pressure. It takes longer for air to flow over the bottom of a Frisbee, thus creating a higher-pressure area that lifts the Frisbee up into the air. Have students compare airfoil shapes with the wing shapes on different airplanes. Why do different planes have different wing shapes? Students can research aerospace engineers and how they use lift/drag. Activity Scaling (Return to Contents)
References (Return to Contents) This activity is adapted from the Society of Women Engineer's Internet Activity Center: http://www.swe.org/iac/LP/wind_01.html Owner (Return to Contents) Integrated Teaching and Learning Program, College of Engineering, University of Colorado at BoulderContributors Tom Rutkowski, Alex Conner, Geoffrey Hill, Malinda Schaefer Zarske, Janet YowellCopyright © 2004 by Regents of the University of Colorado.The contents of this digital library curriculum were developed under a grant from the Fund for the Improvement of Postsecondary Education (FIPSE), U.S. Department of Education and National Science Foundation GK-12 grant no. 0226322. However, these contents do not necessarily represent the policies of the Department of Education or National Science Foundation, and you should not assume endorsement by the federal government. Last Modified: April 27, 2006
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