8.4 Flashcards

1
Q

What’s the difference between manoeuvrability and controllability

A

Manoeuvrability- The quality of an aircraft that allows it to be manoeuvred easily and to withstand the stresses imposed by manoeuvres.

Controllability- The capability of an aircraft to respond to the pilot’s control, especially regarding flight path and attitude.

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2
Q

What movement does yaw act on and what axis is it stable on

A

Acts on Vertical
Stable on vertical

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3
Q

What axis does roll act on and what axis is it stable on

A

Acts on Longitudinal
Stable on lateral

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4
Q

What axis does pitch act on and what axis is its stability along

A

Acts on lateral
Stable on longitudinal

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5
Q

What’s static stability

A

Refers to the initial tendency of the aircraft to return back to a position of equilibrium

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6
Q

What’s the difference between a positive, neutral and negative static stability

A

Positive tends to return back to its initial state of equilibrium after being disturbed

Neutral tends to stay at its new attitude when it’s been disturbed

Negative tends to continue to move away from its original attitude when it’s been disturbed

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7
Q

What’s dynamic stability

A

Refers to ossicliations of aircraft after a aircraft movement has occurred

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8
Q

What’s positive dynamic stability, neutral, negative

A

Positive is a oscillation that dampen out over time and returns to its equal state

Neutral is an oscillation that will remain and never dampen out

Negative is oscillations that will worsen over time

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9
Q

What’s longitudinal stability

A

The tendency of the aircraft to go nose up or down around the lateral axis

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10
Q

What 3 factors does longitudinal stability dependent on

A

Location of the wing with respect to the centre of gravity

Location of the horizontal tail surfaces with respect to the centre of gravity

Area or size of the tail surfaces

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11
Q

How does the difference between the centre of gravity and the aerodynamic centre affect the longitudinal stability

A

Is the difference is big then the stability is high and if it’s small then the stability is low

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12
Q

What axis does directional/weathercock stability work along

A

The vertical axis

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13
Q

What two things does the directional stability depend on

A

The fin of the aircraft
Sweep back angle

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14
Q

How do aircraft help to better there directional stability

A

By increasing the the surface area behind the c of g
By sweeping wings

Done using dorsal fin or keel surface

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15
Q

What axis does lateral stability work about

A

The longitudinal axis

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16
Q

What. 4 things can be done to make the aircraft laterally stable

A

Dihedral
Sweep-back
Keel effect
Weight distribution

17
Q

What’s sideslip

A

The angle between ac centre line and the sideslip direction

18
Q

What acts as the keel on aircraft

A

The fuselage

19
Q

When does spiral dive occur

A

When there’s greater affect on direction stability than lateral

20
Q

When does Dutch roll exist

A

When there’s greater effect on the lateral stability than the directional stability

21
Q

How can Dutch roll be reduced

A

By reducing sweep angle of wings by improving the directional stability

Increasing size of vertical stab but this can have lift and drag affects