The Aerofoil & Lift Flashcards

1
Q

What is an Aerofoil?

A

A part of an aircraft designed to produce lift.

A device which gets a useful reaction from Air moving over its surface

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2
Q

Name some Aerofoils?

A

Wing
Tail surfaces
Propellers

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3
Q

What is the forward rounded part of an Aerofoil called?

A

The leading edge

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4
Q

What is the angle of incidence?

A

The angle at which the wing is attached to the fuselage

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5
Q

The rear part is called?

A

The trailing edge

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6
Q

What is the chord line?

A

It joins the leading and trailing edges

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7
Q

What is the angle of attack (AoA)?

A

The angle formed by the chord line and the relative airflow

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8
Q

What is the longitudinal axis?

A

The line through the fuselage if the aircraft from nose to tail.

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9
Q

What is the aerofoil destined to do?

A

Increase the velocity of the airflow over its top surface, reducing pressure.

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10
Q

What produces lift?

A

A combination of pressure decrease (above) and increase (below the wing) produces lift.

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11
Q

What is laminar flow?

A

The smooth uninterrupted flow of air over the contour of the wings of an aircraft in flight.

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12
Q

What happens in the laminar flow is interrupted?

A

Turbulence is created, resulting in a loss of lift, and increases drag.

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13
Q

What is a laminar aerofoil?

A

An aerofoil designed for minimum drag and a smooth flow over the boundary layer.

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14
Q

What is the angle of attack?

A

The angle between the chord line and relative wind

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15
Q

When is a wing said to be stalled?

A

When the critical angle of attack (AoA) is reached, and the laminar flow breaks away from the wing.

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16
Q

What does stalling result in?

A

A loss of lift and aircraft loses altitude.

17
Q

Can an aircraft stall at any speed and attitude. True or False?

A

True

18
Q

Does weight, airspeed or dynamic pressure effect the critical AoA?

A

No it remains the same regardless. Depends on the design of the wing.

19
Q

What is normally the critical angle of a given aircraft?

A

(Typical 15 degrees)