Stability Flashcards

1
Q

When an object is disturbed and returns to its original path but in doing so it starts to oscillate at an increasing rate it is said to be statically —— and dynamically ——

A

Stable
Unstable

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

A dynamic stability function can exist only if there is —— stability.

A

Static

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

Most helicopters, stick held, are statically ——- and dynamically ——-. Stick free most helicopters are statically ——- and there( can, can not)be a dynamic function under those circumstances.

A

Stable
Unstable
Unstable
Cannot

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

Longitudinal stability is in the ——- plane around the (longitudinal, lateral, normal) axis. Lateral stability is in the ——- plane around the (longitudinal, lateral, normal) axis. Directional stability is in the ——- plane around the (longitudinal, lateral, normal).

A

Pitching
Lateral
Rolling
Longitudinal
Yawing
Normal

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

Stick held, when a gust of wind strikes a helicopter on the nose during a hover,dynamic (stability, instability) will cause it to oscillate forward and back at a (reducing, increasing) rate.

A

Instability
Increasing

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

The main function of a stabiliser is to dampen out (static, dynamic)oscillations. In rearward flight it has a (positive, negative) influence on longitudinal stability.

A

Dynamic
Negative

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

Synch elevators (can, cannot) pitch up/down, they respond to cyclic ( fore/aft, left, right) movements only.

A

Can
Fore/aft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

Beyond a certain speed in forward flight, most helicopters are directionally statically —— and dynamicaly ——-.

A

Stable
Stable

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

Control power is a function of the effectiveness of ( collective, cyclic)to achieve changes in fuselage attitude. Generally the rigid rotor has (most, least) control power, the semi rigid rotor has (most, least)

A

Cyclic
Most
Least

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Offset flapping hinges( do, do not) assist in keeping the fuselage parallel with the rotor disc and they allow a (wider, narrower) range of centre of gravity position.

A

Do
Wider

How well did you know this?
1
Not at all
2
3
4
5
Perfectly