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M8.2 Airflow Fundamentals

Total questions: 12

Worksheet time: 12mins

Name
Class
Date
1.

What disrupts laminar flow over a wing?

a)

Smooth surfaces

b)

Surface distortions

c)

High pressure

d)

Low velocity

2.

What is Free Stream Flow?

a)

The flow of air directly affected by the aircraft

b)

Fluid far enough away from a moving body unaffected by it

c)

The direction of airflow with respect to the object

d)

A region where the velocity of the relative airflow is zero

3.

What type of boundary layer is more energetic and resists negative pressure gradients better?

a)

Laminar

b)

Turbulent

c)

Transitional

d)

Stationary

4.

What is the role of stall warning devices in heavier aircraft?

a)

To increase speed

b)

To reduce drag

c)

To alert pilots of potential stalls

d)

To enhance lift

5.

What happens when a wing stalls due to high pressure drag?

a)

It increases speed

b)

It increases lift

c)

It slows the aircraft and the stall increases

d)

It enhances fuel efficiency

6.

What is the term for the airflow returning to its original state after passing over the aerofoil?

a)

Upwash

b)

Downwash

c)

Stagnation

d)

Vortex

7.

What must be considered on a finite wingspan in addition to the bound vortex when considering the air flow around an aerofoil?

a)

Wing-tip vortices

b)

Leading edge vortices

c)

Trailing edge vortices

d)

Stagnation vortices

8.

What is the span-wise element created by the pressure differential?

a)

Towards the root on the top surface of the wing

b)

Away from the root on the top surface of the wing

c)

Towards the tip on the upper surface of the wing

d)

Away from the tip on the lower surface of the wing

9.

What is the primary function of winglets on an aircraft?

a)

To reduce wingtip vortices

b)

To decrease aircraft weight

c)

To increase fuel consumption

d)

To enhance passenger comfort

10.

How does a turbulent boundary layer affect the drag on an aircraft?

a)

It increases drag

b)

It has no effect on drag

c)

It decreases drag

d)

It stabilizes drag

11.

What is the effect of increasing the angle of attack on a wing?

a)

It has no effect on lift

b)

It reduces fuel efficiency

c)

It increases lift until a critical angle

d)

It decreases lift

12.

What is the primary cause of induced drag on an aircraft?

a)

High speed

b)

Engine thrust

c)

Wingtip vortices

d)

Low altitude