Theory of Flight Flashcards

1
Q

List the parts of a fixed wing aircraft

A
Rudder
Elevators 
Ailerons
Trim Tabs
Flaps
Slats
Fuselage
Landing gear
Tail-plane
Vertical Stabiliser
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2
Q

What are Trim Tabs?

A

Secondary flight control surface, located at the end of the elevator, that aids in maintaining the set attitude without further control input.

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3
Q

What are Slats?

A

Secondary flight surface, located on the inside front wing, that helps maintain the laminar when the angle of attack is increased.

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4
Q

Define Angle of Attack

A

The angle between the relative wind and the chord line of the wing.

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5
Q

What are Flaps

A

Secondary flight surface, located on the inside rear wing, that help maintain lift at low speeds by increasing the camber.

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6
Q

Define Camber

A

The convexity of the curve of an aerofoil from the leading edge to the trailing edge.

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7
Q

List the types of wing

A
Low 
Mid 
High
Gull
Inverted Gull
Anhedral
Dihedral
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8
Q

What is the Bernoulli principle ?

A

As air moves over an aerofoil the pressure above is lesser than the pressure below, this in turn causes the aerofoil to be pushed up creating lift.

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9
Q

What forces affect flight?

A

Weight
Thrust/Power
Lift
Drag

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10
Q

What is lift?

A

An aerodynamic force generated by an aerofoil’s motion through the air.

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11
Q

What is drag?

A

An aerodynamic force that opposes an aircraft’s motion through the air and is generated by every part of an aircraft.

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12
Q

What is thrust?

A

A mechanical force, provided by a system of propulsion, which moves the aerofoil through the air.

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13
Q

What is weight?

A

The force generated by the gravitational attraction of the earth on the aircraft.

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14
Q

What are the parts of a rotary wing aircraft?

A
Wings
Tail-plane
Tail-rotor
Tail-boom
Undercarriage
Cabin
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15
Q

How are helicopters controlled?

A

Cyclic pitching of the rotor blades to move in a direction.
Collective pitching or the rotor blades to climb and descend.
Pitching of the tail rotor blades to change facing direction.

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16
Q

What factors affect aircraft performance?

A
Maximum Speeds
Stall Speeds
Ceiling
Airflow – Streamline (or laminar) flow, Turbulent flow
Angle of Attack
17
Q

Define Stalling Speed

A

The minimum speed at which flight can be maintained.

Increases with altitude due to decrease in density.

18
Q

What is Vy?

A

The speed for best rate of climb (ROC) – the least amount of time to climb

19
Q

What is Vx?

A

The speed for best angle of climb (AOC) - the least distance to climb.

20
Q

Define Service Ceiling

A

The altitude at which no additional speed will cause an increase in altitude

21
Q

Define Zero Rate of Climb

A

Where an aircraft cannot climb further without an increase in speed.

22
Q

Define Laminar

A

Air flowing smoothly over the upper wing surface.

23
Q

Define Boundary Layer

A

Where flow separation occurs between the wing and the laminar.

24
Q

Define Flow Seperation

A

A loss of laminar flow causing a loss of lift that can lead to stalling.

25
Q

List the speed performance Vat categories:

A
A - Less than 91 kts
B - 91 to 120 kts
C - 121 to 140 kts
D - 141 to 165 kts
E - 166 to 210 kts
26
Q

What is Vat?

A

1.3 times the stall speed in landing configuration at the maximum certified landing mass