Category EA P09 Rocket Science: The Wings to Fly

Abstract This science fair project explores the study of rocket wing

aerodynamics. It involved comparing twelve different wing shapes and

sizes to see which would create the least amount of drag. This would

indicate which type of wing would fly the best because of its ability to cut

through the wind. The hypothesis was, if the rocket’s wings are large and

rounded, then they will have the least amount of drag. The variable in this

project was wing size and shape. The control was a wingless rocket.

Each rocket had three wings and was tested using a homemade milk

carton wind tunnel. In total, thirty-six wings were constructed and used in

this project. Twelve of the wings were triangle shaped, another twelve

were four-sided, and the last twelve were rounded. Each set of shapes

had various wing sizes labeled A, B, C, or D, noting largest to smallest.

The rockets were tested keeping the wing speed constant. The amount of

drag was calculated using the equation: drag= (tanx°)(9.81)(mass in kg).

After running six trials for every wing shape and size, the hypothesis was

disproven and unsupported by the data. In fact, the size D triangle wing

created the smallest amount of drag. This project is a useful discovery in

the field of aerodynamics because if small-scale triangle wings fly the

best, rocket scientists should be able to incorporate them into newer

designs of rockets, proving to make them more efficient. The concept may

even be applied to airplanes, though the design would have to face slight

modifications.

Bibliography Benson, T. (2010, August 10). The Drag Equation. National Aeronautics

and Space Administration. Retrieved August 26, 2010, from

http://www.grc.nasa.gov/WWW/K-12 /airplane/drageq.html>



Jones, Larry. (2009, June 27). Physics Information. Journey into Science.

Retrieved July 9, 2010, from

http://www.sciencebyjones.com/physics_definitions.htm>



Lanese, Tina. (2007, March 21). Rocket Aerodynamics. Science Buddies.

Retrieved July 8, 2010, from http://www.sciencebuddies.org/science-fair-

projects/project_ideas/Aero_p002. shtml>



Scott, Jeff. (2003, November 23). Rocket Nose Cones and Altitude.

Aerospaceweb.org. Retrieved August 12, 2010, from

http://www.aerospaceweb.org/question/aerodynamics /q0151.shtml>
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