Stability Flashcards

1
Q

Static stability

A

Initial response of the a/c

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2
Q

Dynamic stability

A

Change over time

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3
Q

Statically neutral

A

Push the ball and remains where it is pushed

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4
Q

Positive static

A

Pushed the ball it wants to return to original position

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5
Q

Negative static

A

Push the ball, it will continue to roll

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6
Q

2 different types of dynamic stability

A

A-periodic without oscillation

Periodic with oscillation

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7
Q

Neutral dynamic and static

A

Remains in the position it was pushed to

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8
Q

Positive static and neutral dynamic

A

Tries to get back to equilibrium but it doesn’t get better and it doesn’t get worst, constant oscillations at the same heights

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9
Q

Positive static and negative dynamic

A

Tries to get to equilibrium but the oscillations get worst over time

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10
Q

Negative static, negative dynamic

A

Continues to get worst

A-periodic

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11
Q

Longitudinal stability

A

Stability in the pitch

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12
Q

Lateral stability

A

Stability in the roll

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13
Q

Directional stability

A

Yaw

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14
Q

Point on the wing where the force acts

A

AC

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15
Q

M Cm

A

Pitching moment
Lateral axis
Positive is up

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16
Q

L Ci

A

Rolling moment
Longitudinal axis
Positive is right

17
Q

N Cn

A

Yawing moment
Normal axis
Positive is right

18
Q

How can you change the tail plane to make it more stable

A

Increase the surface area

Move the tailplane further away

19
Q

Further aft CG

A

Decreases stability

20
Q

Further fwd CG

A

Increases stability

21
Q

Directional stability

A

Stability in the yaw

Airflow to the side of the nose, a/c will want to yaw into the airflow as it hits the tail

22
Q

To improve directional

A

Increase the size of the tail

Increase the distance of the tail from the CG

23
Q

Lateral stability

A

All about the wings

24
Q

Lateral - AoA of the wings

A

Upgoing, Reduced, wants to pitch down

Downgoing, increases, wants to pitch down

25
Improving lateral stability
Low mounted wing has to be dihedral to make it more stable High mounted wing has to be anhedral to reduce the dihedral effect Increase the sweepback A keel surface above the CG
26
Decreases lateral stability
Anhedral wings A keel below the CG will destabilise - vortral fins Low wings
27
Longitudinal stability
Disturbance in the pitch
28
Absolute AoA
From the RAF to the zero lift line Using absolute AoA makes it easier to determine the reaction force
29
Cm formula and was is it and the most important factor
Cm = m/qsL Natural ability for the a/c to pitch in response to a disturbance Most dominant is IAS square (q) which means the faster we go the less Cm
30
In S and L with a reduction in speed, what must be done to the elevator and trim tab to make the stick force 0
Elevator is deflected upwards, trim tab further downwards
31
Which direction does a bob weight move the control stick
Forwards
32
The level of effect on stick force by a change in speed from a trimmed position
High speed small change in speed = less effect on stick force Low speed small change in speed = bigger effect on stick force
33
For an a/c to exhibit static longitudinal stability where do you want the lift to act
Aft of the CG, extra lift will push the nose down again Fwd of the CG, the extra lift will push the nose further up
34
Why is excessive lateral stability undesirable for transport a/c
During sideslip, e.g during a cross wind, it may impose excessive demands on roll control
35
Reducing sweepback
Decreases static lateral stability
36
On fully powered controls what happens to the neutral position of the control column when trimming
Remains unchanged