Aerodynamics 1 Flashcards

1
Q

What effect does weight have on glide range?

A

No effect - glide perf is based on lift-drag ratio.

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2
Q

What effect does weight have on rate of descent?

A

The heavier the ac, the greater its ROD. Due to ac having a higher speed for a given rate of descent.

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3
Q

What is the aerofoil chord line?

A

A straight line from leading edge to the trailing edge of the aerofoil

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4
Q

What is the mean chord line?

A

Wing area divided by wing span.

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5
Q

What is the angle of attack?

A

Angle between the chord line and relative airflow.

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6
Q

What is the coefficient of lift?

A

The lifting ability of a particular wing

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7
Q

What 2 things does the coefficient of lift depend on?

A

Shape of the wing and the angle of attack

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8
Q

Where does the centre of pressure move with a higher angle of attack?

A

Closer to the leading edge

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9
Q

Describe aspect ratio?

A

Aspect ratio is the ratios of the wing’s span to its geometric chord.

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10
Q

What are the two types of drag?

A

Profile drag

Induced Drag

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11
Q

What is profile drag also known as?

A

Zero-lift drag

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12
Q

What is profile drag comprised of?

A
  1. Form or pressure drag
  2. Skin-friction drag
  3. Interference drag
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13
Q

What is VIMD?

A

The speed at which induced and profile drag are equal.

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14
Q

What causes wingtip vortices?

A

Spanwise airflow over the upper and lower surface of the wing.

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15
Q

What are the effects of span wise airflow over a wing?

A

Creates wing-tip vortices
Reduced aileron efficiency
Reversed span wise airflow increases disturbed airflow on the upper surface at the tip - contributes to wingtip stall.

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16
Q

What is the purpose of vortex generators/fences?

A

To reduce span wise flow.

17
Q

What are winglets designed to do?

A

Reduce induced drag

18
Q

What limits an ac CG?

A

The ability of the tailplane to generate lift.

19
Q

How does weight effect the descent point?

A

The heavier the aircraft the earlier its descent point due to momentum.

20
Q

What are the 2 main advantages for jet aircraft having swept wings?

A
  1. High mach cruise speeds

2. Stability in turb

21
Q

What are the four disadvantages of a swept wing?

A
  1. Poor lift qualities
  2. Higher stall speeds
  3. Speed Instability
  4. A wing tip stalling tendency.