8.4 Flight Stability and Dynamics Flashcards

1
Q

What is meant when referring to stability?

A

We refer to how the aircraft is able to follow a

planned straight and level course without pilot action

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2
Q

What are the two types of stability?

A

Static stability

Dynamic stability

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3
Q

What is meant by negative static stability?

A

An object when disturbed tends to continue in the displacement direction

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4
Q

What is meant by neutral static stability?

A

When displaced the object will not show any tendency to move back or move away from its original position

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5
Q

What is meant by positive static stability?

A

The object when disturbed will tend to return to its

original point of equilibrium

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6
Q

When does dynamic stability apply?

A

It only applies if the object has positive static stability

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7
Q

If it assumed that there are no friction forces, an object that oscillates forever after displacement, what is this effect called?

A

An undamped oscillation

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8
Q

If we assume friction forces, an object that is displaced that eventually damps out is called?

A

A damped oscillation, it is dynamically stable

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9
Q

Explain negative dynamic stability

A

If a ball is disturbed, and continues to depart away from its original equilibrium position, a divergent oscillation is formed , this is dynamically unstable

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10
Q

What occurs if an objects c of g and its pivot point are in the same place?

A

The object will have neutral stability and will not return to its original position

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11
Q

What does an object have if its pivot point is below the c of g?

A

Negative static stability, a disturbance will cause the object to move further away from its original position

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12
Q

What does an object have if its pivot point above the c of g?

A

The object will return to its original position should it be disturbed

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13
Q

What influences stability?

A

The distance between the pivot point and the c of g

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14
Q

What is the effect of a large distance between the pivot point and the c of g?

A

The longer the distance the greater the stability, and thus the tendency to return to its original position is directly linked to this length

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15
Q

With dynamic stability, describe positive stability

A

(damped) the aircraft will eventually return to the original attitude

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16
Q

With dynamic stability, describe negative stability

A

(divergent) the aircraft will continue to experience larger and large oscillations

17
Q

With dynamic stability, describe neutral stability

A

(un-damped) the aircraft will continue on its new trajectory, not getting ant worse or better with regards to oscillations

18
Q

What are the three aircraft axis?

A

Lateral
Longitudinal
vertical

19
Q

Which axis deals with roll?

A

longitudinal (roll)

20
Q

Which axis deals with pitch?

A

lateral ( pitch )

21
Q

Which axis deals with yaw?

A

Vertical ( directional )

22
Q

What axis is directional/weathercock?

A

The vertical

23
Q

What affects the directional stability?

A

The fin of the aircraft and on the sweepback of the wing

24
Q

What happens to the fin when it has been deflected in flight?

A

The fin on one side has a higher pressure than the other, the subsequent turning motion behind the c of g is greater than the turning moment in front of the c of g, causing the aircraft to return to its original flight path

25
Q

What additional surfaces can be fitted to an aircraft to increase directional stability?

A

Keel surface and dorsal fin

26
Q

Describe the effect of swept swings on directional stability

A

When an aircraft is displaced and a yawing motion occurs, the forward going wing presents a larger surface to the relative airflow, this increases its drag, this additional drag then creates the opposing yaw required to bring the aircraft back on track

27
Q

lateral stability acts around the … what axis?

A

Longitudinal

28
Q

Effect of dihedral when the aircraft is disturbed?

A

The angle of the each wing heading into the relative airflow is different, the down going wing has a higher angle of attack, the up going wing has a lower angle of attack, this creates less lift on the upwards wing and more lift on the down going wing, this creates a tendency for the aircraft to return itself to the original attitude

29
Q

Directional stability acts around the … what axis?

A

vertical, normal, yaw

30
Q

What is side slip angle?

A

The angle between the aircraft centre line and the slip direction

31
Q

When in a slip, where is the wind?

A

Opposite to the slip direction

32
Q

When in a slip, which wing creates more lift?

A

The wing in the slip direction

33
Q

When is the effect of a spiral dive strongest?

A

When there is a greater effect on directional stability than lateral

34
Q

When is Dutch roll likely to occur?

A

When there is a greater effect on lateral than directional stability

35
Q

How can you partially overcome Dutch roll?

A

By having less of a sweep angle, and by improving directional stability

36
Q

How can you improve the directional stability?

A

By having a bigger fin, at the cost of added weight and increased drag