Revision : Basic Aerodynamics

Revision : Basic Aerodynamics

University - Professional Development

20 Qs

quiz-placeholder

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Revision : Basic Aerodynamics

Revision : Basic Aerodynamics

Assessment

Quiz

Other

University - Professional Development

Medium

Created by

nuraina mardhiah

Used 38+ times

FREE Resource

20 questions

Show all answers

1.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

In which atmospheric layer is the temperature assumed to be constant at -56.5°C?

Ionosphere

Lower stratosphere

Troposphere

2.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Humidity is a condition of moisture and dampness. With the increase in temperature, the humidity will

increase

decrease

be unaffected

3.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Aircraft design ensures that turbulent flow on top of the wing is limited to a minimum, so that

the drag can be reduced

the stall angle can be increased

the lift coefficient can remain constant

4.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

How does the air flow behave when passing through a convergent / divergent duct?

The airflow accelerates as it leaves the throat

The airflow accelerates as it enters the throat

The airflow decelerates as it enters the throat

5.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

The first layer of the Boundary Layers which is in contact with the airfoil surface is static. In the upper layers, the velocity of air increases. This is effect is due to:

A greater pushing force from relative wind

The viscosity of the air

The compression of upper layers of air

6.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Viscosity is defined as

The tendency of one layer of fluid to stick to the next layer, preventing relative motion

Friction due to roughness of the surface, preventing relative motion

A property of air flow to become turbulent at higher speeds

7.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Which of the following explains the effect of aileron reversal?

The aircraft tends to yaw in the opposite direction

The aircraft tends to roll in the opposite direction

The aircraft tends to pitch in the opposite direction

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