Module 4 Stability and Control Flashcards

1
Q

Roll movement which axis?

A

Longitudinal Axis

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2
Q

Pitch movement which axis?

A

Lateral Axis

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3
Q

Yaw movement which axis ?

A

Vertical Axis

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4
Q

Lateral stability is stable in ?

A

Roll (longitudinal axis)

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5
Q

Longitudinal stability is stable in?

A

pitch ( lateral axis )

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6
Q

Directional stability is stable in?

A

yaw (vertical axis)

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7
Q

Movement around the longitudinal Axis is called ?

A

Roll

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8
Q

Movement around the vertical axis is called?

A

Yaw

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9
Q

Movement around the lateral axis is called?

A

Pitch

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10
Q

Primary Flight control for longitudinal axis movements is called ?

A

Ailerons

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11
Q

Primary flight control for lateral axis movements is called?

A

Elevators

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12
Q

Primary flight control for vertical axis Movement is called?

A

Rudder

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13
Q

Longitudinal movement the stability is provide by ?

A

Wings

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14
Q

Lateral movements the stability is provide by ?

A

Horizontal stabilizer

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15
Q

Vertical movements the stability is provide by ?

A

Vertical stabilizer

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16
Q

The stability about the Longitudinal axis is called

A

Lateral

17
Q

The stability about Lateral axis is called

A

Longitudinal

18
Q

the stability about the vertical axis is called

A

Directional

19
Q

What are the two types of stability

A

Static stability

Dynamic stability

20
Q

What is static stability?

A

Is the initial tendency that the A/C displays after its equilibrium is disrupted

21
Q

Types of static stability?

A

Positive, neutral and negative

22
Q

What is Adverse yaw ?

A

created during a roll induced turn, increase drag on the outside wing

23
Q

Ways to control the yaw?

A

–Aileron/rudder interconnect
–Frise ailerons
–Differential ailerons
–Roll spoiler

24
Q

What is dutch roll?

A

Aircraft tends to wander about the roll and the yaw axes at the same time

25
Q

Types of Canards

A

Control and Lifting

26
Q

What is Dynamic stability

A

Describes the tendency of oscillate after its equilibrium is disrupted

27
Q

Tail design helps with?

A

Directional stability = vertical stabilizer and rudder

28
Q

Stability does not refer to the axis of the aircraft but rather the ?

A

Behaviour