Aerodynamics, AOA, Stalls, Spins, Gnd Effect, Turns

Aerodynamics, AOA, Stalls, Spins, Gnd Effect, Turns

12th Grade

16 Qs

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Aerodynamics, AOA, Stalls, Spins, Gnd Effect, Turns

Aerodynamics, AOA, Stalls, Spins, Gnd Effect, Turns

Assessment

Quiz

Other

12th Grade

Hard

Created by

Rick Chapman

Used 1+ times

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16 questions

Show all answers

1.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

The four forces acting on an airplane in flight are

lift, weight, thrust, and drag.

lift, weight, gravity, and thrust.

lift, gravity, power, and friction.

2.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

When are the four forces that act on an airplane in equilibrium?

During unaccelerated level flight.

When the aircraft is accelerating.

When the aircraft is at rest on the ground.

3.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What is the relationship of lift, drag, thrust, and weight when the airplane is in straight-and-level flight?

Lift equals weight and thrust equals drag.

Lift, drag, and weight equal thrust.

Lift and weight equal thrust and drag.

4.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Which statement relates to Bernoulli’s principle?

For every action, there is an equal and opposite reaction.

An additional upward force is generated as the lower surface of the airfoil deflects air downward.

Air traveling faster over the curved upper surface of an airfoil causes lower pressure on the top surface.

5.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

The term “angle of attack” is defined as the angle between the

chord line of the wing and the relative wind.

airplane’s longitudinal axis and that of the air striking the airfoil.

airplane’s center line and the relative wind.

6.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

The angle between the chord line of an airfoil and the relative wind is known as the angle of

lift.

attack.

incidence.

7.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

The angle of attack at which an airplane wing stalls will

increase if the CG is moved forward.

change with an increase in gross weight.

remain the same regardless of gross weight.

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