Aviation 2 Unit 4 Section A & B Quiz Study

Aviation 2 Unit 4 Section A & B Quiz Study

12th Grade

11 Qs

quiz-placeholder

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Aviation 2 Unit 4 Section A & B Quiz Study

Aviation 2 Unit 4 Section A & B Quiz Study

Assessment

Quiz

Other

12th Grade

Practice Problem

Medium

Created by

Anthony Mellendorf

Used 2+ times

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11 questions

Show all answers

1.

MULTIPLE SELECT QUESTION

30 sec • 1 pt

The overall lift of an airfoil is dependent on what two factors? Select all that apply

Airspeed
Angle of Attack (AOA)
Air Density
Velocity

2.

MULTIPLE SELECT QUESTION

30 sec • 1 pt

What factors affect the coefficient of lift? (Select all that apply)

Camber of an airfoil
Velocity of an airfoil
Weight of an airfoil
Thickness of an airfoil

3.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

The wing tip of an airfoil is designed to stall after the wing root, allowing the ailerons to be effective

True
False
Do not answer
Do not answer

4.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

The Angle of Attack (AOA) at which an airfoil of an aircraft stalls is constant

True
False
Do Not Answer
Do Not Answer

5.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What variable is constant in the lift equation?

Lift
Velocity
Surface Area
Air Density

6.

MULTIPLE SELECT QUESTION

30 sec • 1 pt

What increases the lift of an airplane (Select all that apply)

Increasing the surface area
Increasing the camber of the wing
Increasing the weight of the airplane
Decreasing the density of the air

7.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

The angle of attack (AOA) of an airfoil is the angle between the leading edge and the relative wind flow

True
False
Do not pick
Do not pick

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