Oral Exam/ Aerodynamics Flashcards

1
Q

What are the four forces of flight?

A

Lift Weight Thrust Drag

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2
Q

How is lift created?

A

Airfoils accelerate airflow downward – this is an example of Newton’s 3rd law
Bernoulli’s Principle – high speed air over the upper surface creates low pressure while low speed air beneath the wing creates high pressure. Low pressure above the wing is a essentially a suction force that keeps an airplane aloft. High pressure below the wing seeks to equalize the low pressure area above by pushing up against the airfoil and also contributes to lift.

o Air traveling faster over a curved upper surface causes lower pressure
on the top surface, pulls wing up.
o High pressure air underneath the wing tries to get to the upper portion
of the wing, creating lift.

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3
Q

Explain the different types of drag

A

Parasite- increases with speed
form: shape in air
interference: opposing features combining
skin friction drag: material

Induced – byproduct of lift

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4
Q

Describe the various components of an airfoil

A

Leading/trailing edge
Upper/lower camber
Chord line
Relative wind
Angle of attack

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5
Q

What is camber?
Can we change it?

A

Curvature of the wing – it can be changed by extending/retracting flaps

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6
Q

Explain Bernoulli’s Principle

A

As velocity of a fluid or air increases, the pressure decreases. High speed air over the upper surface creates low pressure while low speed air beneath the wing creates high pressure. High pressure moves upwards towards the lower pressure.

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7
Q

What is angle of incidence? Can we change it?

A

The angle between the wing chord line and the fuselage – it cannot be changed

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8
Q

Explain Stability

A

Lateral stability
Longitudinal stability
Vertical stability
Positive stability
Betrayal stability
Negative stability
Static stability
Dynamic stability

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9
Q

Lateral stability

A

Resistance to roll

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10
Q

Longitudinal Stability

A

Resistance to pitch

relationship of center of gravity to
center of lift.
In small aircraft, center of gravity is in front of center of lift

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11
Q

Vertical Stability

A

Resistance to yaw

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12
Q

Positive Stability

A

Tendency to return to equilibrium

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13
Q

Neutral Stability

A

Tendency to stay in new position

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14
Q

Negative Stability

A

Tendency to continue to move away from equilibrium

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15
Q

Static Stability

A

Initial tendency

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16
Q

Dynamic Stability

A

Response over time

17
Q

Compass errors
magnetic variation

A

Difference between magnetic and true north

18
Q

What do you do if you become lost in-flight?

A

Climb
Circle
Conserve
Confess
Communicate

19
Q

Aircraft is in equilibrium during unaccelerated flight when

A

Thrust = Drag
Lift = Weight

20
Q

Chord line

A

from middle of leading edge to middle of trailing edge of wing

21
Q

Angle of attack

A

angle from the relative wind to the chord line (A).
Angle is acute, less than 90 degrees

22
Q

Laminar flow

A

when air flows smoothly over the win

23
Q

aerodynamic stall

A

angle of attack is too high, the air no longer conforms to the wing and separates

24
Q

Frost

A

• Frost or anything else on a wing will disrupt smooth airflow.
• May prevent the aircraft from becoming airborne at normal takeoff speed.
• May also increase stall speed

25
Q

Aerodynamics of flaps

A

Flaps down increase the drag, allow a steeper approach to landing (angle of
descent) without increasing airspeed.

26
Q

Yaw

A

turning around the vertical axis, controlled by the rudder

27
Q

Roll

A

turning around the longitudinal axis, nose to tail, controlled by
alerions

28
Q

Pitch

A

turning around the lateral axis, side to side, controlled by the elevators

29
Q

Load Factor

A

Banking (turn) increases G forces (the load factor) on aircraft. Compensates
for centrifugal force

30
Q

Pitot-Static Instruments

A

air speed indicator
vertical speed indicator (rate of climb)
altimeter.

31
Q

Clogged pitot tube

A

o Put pitot cover on tube to avoid stuff clogging it
o Pitot heat prevents icing
o Affects air speed indicator only

32
Q

Clogged static vent

A

Affects air speed and vertical speed indicators, and altimeter

33
Q

Compass errors

A

Variation
Deviation
Magnetic dip
Oscillation
Northerly turning errors
Acceleration errors

34
Q

Compass errors
Deviation

A

System affects compass