Paper Airplane Project Glider Design Testing Worksheet Haley Cornelius
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The Science of Flight
Paper Airplane Project Glider Design Testing Worksheet
Tester Name:
Haley Cornelius
Description of Testing Site
The testing site is the Naval Air Station Whidbey Island Air Terminal hangar. There is ample space and height for
paper airplanes to fly and no wind interference.
Distance Design Testing
Name of Distance Design
The Basic Dart
Hypothesis for Distance Design
The Basic Dart will perform well in regard to distance due to its sleek and aerodynamic design. It is thin and narrow
which will reduce the amount of drag force that will act upon it. Weigh twill not really play a role in this experiment
since both designs are required to be made of the exact same material. The Basic Dart will have high wing-loading
due to its small wing area compared to its body mass therefore it may have an issue maintaining the amount of lift
required to perform well in regard to duration. Thrust will be determined by how the thrower launches the paper plane
Thrust Method for Distance Design (be specific!)
With the Basic Dart, the harder it is launched, the faster and farther the plane will travel. It would also be best to throw
it with as much of an upward angle as possible to counteract any drag it will experience.
[NOTE: The three items above were completed in part 1 of the project]
Data and Calculations for Distance Design
Distance Design Wing Loading
(enter values to the nearest tenth in the indicated units of measurement)
Total
Glider
Mass
(g)
WingAre
a
(c
m
2
)
Wing Loading
(g/c
m
2
)
4.5
218.63
0.021
Explanation of the method used for calculating wing area
The wings for the Basic Dart form a triangle on top of a rectangle so I calculated the area by using the standard
formula for the area of a triangle: A= ½ B*H and added the result to area of the rectangle at the bottom which is found
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by using the formula A=L*W. The base of the triangle formed by the wings is 16.5cm, the height of the triangle formed
by the wings is 22.5cm. So, A = ½ (16.5)*(22.5) = 185.63 cm^2. The length of the bottom rectangle is 16.5cm and the
width is 2cm. So, A = (16.5)*(2) = 33cm^2. Then I added the two together (185.63+33). The total wing area is
218.63cm^2.
Distance Design Glide Distance
Measure
the
straight line
distance from take-off point to landing point (point where the glider
strikes the ground).
Enter values to the nearest tenth (one decimal place) of a meter.
Test Glider
Number or
Name
Trial 1
Trial 2
Trial 3
Trial
4
Trial 5
Average
Distance
(meters)
Basic Dart
Pink
10.7
9.8
8.3
10.2
9.5
9.7
Basic Dart
Blue
9.6
8.7
8.3
9.2
9.0
8.9
Basic Dart
Orange
7.0
7.3
7.9
7.1
6.8
7.2
Observations
Basic Dart Pink performed the best by reaching an average distance of almost 1 meter farther than
the other gliders.
Sources of Variability, Uncertainty and Error
Sources of variability, uncertainty, and error could be the way the planes were folded – its
impossible for there to not be any variability from one plane to another. Also, the way it was
thrown each time could cause variability – different speeds and different angle – no matter how
much a person tries to keep it consistent.
Results and Conclusions
Include which plane performed best, i.e., the one with the best average distance
achieved in the testing, and a summary of the specific design features and external
factors that likely influenced the performance of the test planes.
Page 2 of 8
Basic Dart Pink performed the best out of the three different planes. Its average distance
reached almost a meter farther than the others. It’s sleek design allowed it to move quickly
through the air and reach a farther distance than those that were tested specifically for
duration. The tests were conducted indoors so wind did not cause an adverse reaction to its
flight time. This plane performed best when thrown fast and hard and with a slight upward
angle.
Flight Duration Design Testing
Name of Flight Duration Design
The Stealth Glider
Hypothesis for Flight Duration Design
The Stealth Glider will perform well in regard to duration due to its large wing area, but may suffer in regard to
distance because it will experience more drag. Weight will not really play a role in this experiment since both designs
are required to be made of the exact same material. The Stealth Glider will have low wing-loading due to its large
wing area and the fact that it doesn’t have much of a body mass due to its lack of a fuselage so it should be able to
quickly produce lift as well as maintain it throughout the duration of the flight. Thrust will be determined by how the
thrower launches the paper plane.
Thrust Method for Flight Duration Design (be specific!)
With the Stealth Glider, it would be best to launch it with medium thrust and at an upward angle so that it can easily
and quickly produce the lift it will need to sustain flight and overcome any drag that may act upon it.
[NOTE: The three items above were completed in part 1 of the project]
Data and Calculations for Flight Duration Design
Duration Design Wing Loading
(enter values to the nearest tenth in the indicated units of measurement)
Total
Glider
Mass
(g)
Total Wing
Area
(c
m
2
)
Wing Loading
(g/c
m
2
)
4.5
242.9
0.019
Explanation of the method used for calculating wing area
The wings for the Stealth Glider form a trapezoid on top of a rectangle so I calculated the area by using the standard
formula for the area of a trapezoid: A= (½ (a+b))*h and added the result to the area of the rectangle at the bottom
which is found by using the formula A=L*W. The bases of the trapezoid formed by the wings are 21.5cm and 6cm,
and the height of the trapezoid formed by the wings is 7.5cm. So, A = (½ (21.5+6))*(7.5) = 103.125cm^2. The length
of the bottom rectangle is 21.5cm and the width is 6.5cm. So, A = (21.5)*(6.5) = 139.75cm^2. Then I added the two
together (103.125+139.75). The total wing area is 242.88cm^2.
Page 3 of 8
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Duration Design Flight Time
Start the timer when the glider is released and stop the timer when the glider hits the
ground.
Enter flight times to the nearest whole second. Calculate the
average
flight times to the
nearest
tenth
of a second.
Test Glider
Number or
Name
Trial 1
Trial 2
Trial 3
Trial
4
Trial 5
Average
Flight Time
(seconds)
Stealth
Glider Pink
1.2
1.1
1.3
0.9
1.2
1.1
Stealth
Glider Blue
2.2
2.5
2.1
2.6
2.0
2.3
Stealth
Glider
Orange
0.9
1.0
0.8
0.5
0.8
0.8
Observations
Stealth Glider Blue performed extraordinarily better than the other two gliders, staying aloft for an
average of more than a second longer.
Sources of Variability, Uncertainty and Error
Sources of variability, uncertainty, and error could be the way the planes were folded – its
impossible for there to not be any variability from one plane to another. Also, the way it was
thrown each time could cause variability – different speeds and different angle – no matter how
much a person tries to keep it consistent.
Results and Conclusions
Include which plane performed best, i.e., the one with the best average flight time
achieved in the testing, and a summary of the specific design features and external
factors that likely influenced the performance of the test planes.
Stealth Glider Blue performed the best out of the three planes. It was a little bit of a learning
curve figuring out exactly how to throw these and get the best result because throwing them
hard and fast like the basic dart plane was not productive at all. I learned that throwing it softer
with an upward motion allowed it to produce the most lift. In real life, this might be one of those
Page 4 of 8
jets that uses vertical takeoff. The experiment was conducted indoors so wind was not a factor
but if I had been outside I probably could have made the glider stay aloft much longer if I was
able to play the wind to my advantage.
Page 5 of 8
Graphs and Images
Test Glider vs. Average Distance Graph for Distance Design (insert graph HERE)
Test Glider vs. Average Flight Time Graph for Duration Design (insert graph
HERE)
Page 6 of 8
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Page 7 of 8
Insert Photos or Videos of Design Build and Testing HERE
Page 8 of 8
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