Module 4 Stability and Control Flashcards

(28 cards)

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

17
Q

The stability about Lateral axis is called

18
Q

the stability about the vertical axis is called

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
Types of Canards
Control and Lifting
26
What is Dynamic stability
Describes the tendency of oscillate after its equilibrium is disrupted
27
Tail design helps with?
Directional stability = vertical stabilizer and rudder
28
Stability does not refer to the axis of the aircraft but rather the ?
Behaviour