Quiz on Flight Stability and Dynamics

Quiz on Flight Stability and Dynamics

Professional Development

21 Qs

quiz-placeholder

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Quiz on Flight Stability and Dynamics

Quiz on Flight Stability and Dynamics

Assessment

Quiz

Physics

Professional Development

Medium

Created by

pramod dheearj

Used 1+ times

FREE Resource

21 questions

Show all answers

1.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What is the primary characteristic of stability in an aircraft?

The ability to fly at high speeds

The capability to carry heavy loads

The tendency to return to a straight-and-level flightpath

The ability to perform complex maneuvers

2.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Which type of stability refers to the initial tendency of an aircraft to return to equilibrium after being disturbed?

Static stability

Dynamic stability

Directional stability

Lateral stability

3.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What does dynamic stability refer to?

The initial response of the aircraft to control inputs

The aircraft's response over time when disturbed

The ability to maintain altitude

The aircraft's speed during flight

4.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Which of the following is a characteristic of positive static stability?

The aircraft continues away from equilibrium

The aircraft remains in a new condition after disturbance

The aircraft returns to its original state after disturbance

The aircraft oscillates indefinitely

5.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What is the phugoid mode in terms of longitudinal oscillations?

A rapid pitching motion

A large-amplitude variation of airspeed and altitude

A constant speed flight

A type of spin

6.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Which factor does NOT affect static longitudinal stability?

Location of the wing with respect to the CG

Area of the tail surfaces

Weight of the aircraft

Location of the horizontal tail surfaces

7.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What is the primary contributor to directional stability in an aircraft?

The area of the horizontal stabilizer

The engine thrust line

The vertical fin and fuselage area aft of the CG

The wing design

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