AERT3200 GLEIM 1 and 5

AERT3200 GLEIM 1 and 5

University

47 Qs

quiz-placeholder

Similar activities

Principles of flight TEST

Principles of flight TEST

University

50 Qs

CPD222 2/64 Final

CPD222 2/64 Final

University

50 Qs

Aerodynamics Quiz fist 100 pages

Aerodynamics Quiz fist 100 pages

University

42 Qs

Airplanes & Aerodynamics

Airplanes & Aerodynamics

8th Grade - Professional Development

48 Qs

POF 3

POF 3

University

50 Qs

pof 6

pof 6

University

51 Qs

ATRN215 FINAL EXAM 2025

ATRN215 FINAL EXAM 2025

University

50 Qs

Aerodynamics Worksheet

Aerodynamics Worksheet

University

49 Qs

AERT3200 GLEIM 1 and 5

AERT3200 GLEIM 1 and 5

Assessment

Quiz

University

Medium

Created by

Audrey Rice

Used 3+ times

FREE Resource

47 questions

Show all answers

1.

MULTIPLE CHOICE QUESTION

45 sec • 1 pt

One of the main functions of flaps during the approach and landing is to

decrease the angle of descent without increasing the airspeed.

provide the same amount of lift at a slower airspeed.

decrease lift, thus enabling a steeper-than-normal approach to be made.

2.

MULTIPLE CHOICE QUESTION

45 sec • 1 pt

Which is true regarding the use of flaps during level turns?

The lowering of flaps increases the stall speed.

The raising of flaps increases the stall speed.

Raising flaps will require added forward pressure on the yoke or stick.

3.

MULTIPLE CHOICE QUESTION

45 sec • 1 pt

The angle of attack of a wing directly controls the

angle of incidence of the wing.

amount of airflow above and below the wing.

distribution of pressures acting on the wing.

4.

MULTIPLE CHOICE QUESTION

45 sec • 1 pt

Some aircraft are fitted with wing spoilers to decrease

drag

takeoff speed

lift

5.

MULTIPLE CHOICE QUESTION

45 sec • 1 pt

A rectangular wing, as compared to other wing planforms, has a tendency to stall first at the

wingtip, with the stall progression toward the wing root.

wing root, with the stall progression toward the wingtip.

center trailing edge, with the stall progression outward toward the wing root and tip

6.

MULTIPLE CHOICE QUESTION

45 sec • 1 pt

An aircraft airfoil is designed to produce lift resulting from a difference in the

negative air pressure below and a vacuum above the airfoil's surface.

vacuum below the airfoil's surface and greater air pressure above the airfoils surface.

higher air pressure below the airfoil's surface and lower air pressure above the airfoil's surface.

7.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Frost covering the upper surface of an airplane wing usually will cause

the airplane to stall at an angle of attack that is higher than normal.

the airplane to stall at an angle of attack that is lower than normal.

drag factors so large that sufficient speed cannot be obtained for takeoff.

Create a free account and access millions of resources

Create resources
Host any resource
Get auto-graded reports
or continue with
Microsoft
Apple
Others
By signing up, you agree to our Terms of Service & Privacy Policy
Already have an account?