AERT3200 GLEIM 1 and 5

AERT3200 GLEIM 1 and 5

University

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47 Qs

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AERT3200 GLEIM 1 and 5

AERT3200 GLEIM 1 and 5

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Audrey Rice

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47 questions

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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.

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