Lecture 2 Flashcards

1
Q

What makes up the atmosphere?

A

78% Nitrogen
21% Oxygen
1% Other

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2
Q

By _____ feet, half of all the air on the planet is below you and by ____ feet, 75% of all air is below you.

A

18,000
34,000

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3
Q

How does temperature affect the density of air?

A

Air expands when heated

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4
Q

Air is less dense when it is ____ and more dense when it is ____.

A

hot
cold

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5
Q

How does humidity affect the density of air?

A

Water vapor is less dense than air (less dense in high humidity)

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6
Q

Air is less dense when there is ____ humidity and more dense when there is ____ humidity.

A

high
low

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7
Q

How does altitude affect the density of air?

A

Fewer air molecules as you reach higher altitude
Air molecules can spread out more at higher altitudes

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8
Q

Air is less dense at ____ altitude and more dense at ____ altitude.

A

high
low

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9
Q

Air is least dense on ____, ____ days, and at ____ altitude.

Air is most dense on _____, _____ days and near _____.

A

hot
humid
high

cool
dry
sea level

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10
Q

What is a standard day?

A

59°F
Sea level
Zero humidity

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11
Q

What are the four forces on an airplane?

A

Lift
Weight
Thrust
Drag

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12
Q

What is Newton’s 1st Law?

Which force(s) does it apply to?

A

A body at rest will stay at rest until an external force acts on it

Drag

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13
Q

What is Newton’s 2nd Law?

A

A force applied to an object at rest causes it to accelerate in the direction of the force

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14
Q

What is Newton’s 3rd Law?

Which force(s) does it apply to?

A

For every action, there is an equal and opposite reaction

Accounts for 10% of lift
Thrust

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15
Q

What is Bernoulli’s Principle?

A

As the velocity of a fluid increases, the pressure decreases

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16
Q

Does the top or the bottom of the wing have higher pressure?

Why?

A

Pressure is higher on the bottom on the wing

Velocity over the top of the wing is higher and lowers the pressure (Bernoulli’s Principle)

17
Q

What accounts for 90% of the lift of a wing?

What about the other 10%?

A

Bernoulli’s Principle (Bernoulli Effect)

Newton’s 3rd Law

18
Q

How is lift created?

A

The more differential pressure between the top and the bottom of the wing, the more lift is produced

19
Q

What is the Coanda Effect?

A

A moving stream of fluid in contact with a curved surface will follow the curvature of the surface rather than continue traveling in a straight line

20
Q

How can you increase the camber shape of the airflow?

How can a higher camber help?

A

Increasing the AOA of the wing

More camber = more lift

21
Q

List some things that can disturb airflow on the leading edge of a wing

A

Rivet heads
Bolts
Dents
Ice formation

22
Q

What is the center of pressure?

A

Lowest air pressure on the top of the wing, or the greatest pressure differential between the top and bottom

23
Q

Lift acts _____ from the _____.

Weight acts _____ from the _____.

A

upward
center of pressure

downward
center of gravity

24
Q

Where is the center of gravity in relation to the center of pressure?

A

CG is slightly forward of the CP

25
Q

What is the center of gravity?

A

Mathematical collection of where weight is applied

26
Q

What are the five parts of an airfoil?

A

Leading edge
Trailing edge
Upper camber
Lower camber
Chord line

27
Q

What is the chord line?

Does it have to be inside the wing?

A

A straight line from the leading edge to the trailing edge

No

28
Q

What is camber?

A

The curvature of the wing
The curvature of the air over or under the wing

29
Q

What is span?

What is chord?

What is aspect ratio?

A

Length of a wing

Width of a wing

Span divided by chord

30
Q

What is the dihedral angle?

What is the purpose of it?

A

The angle of the wing from wing chord to wing tip in relation to the ground

Stability

31
Q

What is the mean camber line?

Which side of this line is positive?

A

Average camber line
Created by subtracting chord line to lower camber from chord line to upper camber

Above the line is positive
Below the line is negative

32
Q

What is the mean aerodynamic chord?

A

The distance between the leading and trailing edge of a wing measured parallel to normal airflow over the wing

33
Q

Why do we care where maximum camber is located?

A

Correlates to the location of lowest pressure (center of pressure)
We need to keep the center of gravity in front of the center of pressure to keep the aircraft stable