Aerofoil Terminology Flashcards

1
Q

What is the Leading Edge?

A

The most forward point on the aerofoil.

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2
Q

What is the Trailing Edge?

A

The most rearward point on an aerofoil.

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3
Q

What is the Upper Surface on an Aerofoil?

A

The top side of the aerofoil.

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4
Q

What is the Lower Surface on an Aerofoil?

A

The bottom side of the aerofoil.

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5
Q

What is Relative Airflow (RAF) ?

A

The air where pressure, temperature and relative velocity are unaffected by the passage of the aircraft.

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6
Q

What is Lift?

A

The component of the Total Reaction that is perpendicular (90°) to the flight path or RAF.

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7
Q

What is Drag?

A

The component of the Total Reaction that is in the same direction and parallel to the RAF.

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8
Q

What is Total Reaction?

A

The resultant of all aerodynamic forces acting on the wing or aerofoil section.

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9
Q

What is the Chord Line?

A

The shortest distance between the leading and trailing edge of an aerofoil.

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10
Q

What is the Mean Camber Line?

A

A line joining the leading and trailing edges of an aerofoil.

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11
Q

Maximum Camber?

A

The point where there is the maximum distance between the mean camber line and the chord line.

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12
Q

How is Maximum Camber expressed?

A

A ratio of the maximum distance between the mean camber line and the chord line.

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13
Q

How is the maximum thickness expressed?

A

A ratio of thickness to the chord length.

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14
Q

What is the Centre of Pressure?

A

The point, usually in the Chord Line through which, the Total Reaction may be considered to act.

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15
Q

What is the Centre of Gravity?

A

The point within the aircraft where the weight acts.

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16
Q

Why is the position of the Centre of Gravity important?

A

It is very important that the CG is in the correct position so the aircraft is balanced.

17
Q

What is the Angle of Attack (a)?

A

The angle between the Chord Line and the flight path or RAF.

18
Q

What is Aspect Ratio?

A

The relationship between the length and the width of a wing.

19
Q

How to calculate Aspect Ratio for a tapered or elliptical wing?

A

Dividing the square of the wingspan by the wing area

AR = Span2 / Wing Area

20
Q

How to calculate the Aspect Ratio for a simple rectangular wing?

A

Divide the wingspan by the chord

AR = wingspan / chord