Stability 😱 Flashcards

(60 cards)

1
Q

What increases longitudinal stability

A

Larger tailplane area

Further forward cg

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2
Q

What does reduced stability do to manoeuvrability and controllability

A

Increases manoeuvrability but reduces controllability

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3
Q

Where does the aerodynamic centre need to be for it to be stable

A

Behind the cg

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4
Q

What does forward cg do to drag

A

Increase trim drag

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5
Q

What is absolute AOA

A

Angle between zero lift line and the raf

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6
Q

What is the most significant factor for pitching coefficient

A

Dynamic pressure

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7
Q

What type of gradient will a longitudinally stable aircraft have

A

Negative

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8
Q

What is the most important contributor to longitudinal stability

A

Tailplane

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9
Q

What is the area of the tailplane and the distance from aircraft cg collectively known as

A

Tail volume

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10
Q

What effect does the fuselage have on the stability of a aircraft

A

Destabilised

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11
Q

Do the engine nacelles have a stabilising or destabilising effect

A

As AOA increases air catches on the lips of the intake = upwards moment = less stable

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12
Q

How does cg position in relation to engines affect stability

A

Closer cg is to engines = less instability

Further away cg is to engines = more instability

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13
Q

What is a static margin

A

Safety margin between the neutral point and aft cg

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14
Q

What affect do trailing edge flaps THEMSELVES have on the stability

A

Stabilise

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15
Q

What effect do flaps have on the overall stability of the aircraft

A

Increase in downwash

= reduced effectiveness at tailplane

= less stable

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16
Q

How does flaps affect the neutral point

A

Flaps extended results in neutral point further forward resulting in reduced longitudinal static stability

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17
Q

What is stick position stability

A

The position you expect the stick to be in for a certain phase of flight

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18
Q

What would be a unstable stick position stability

A

Push forward when you slow down and want to increase AOA

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19
Q

Does trim affect stick position stability or over all stability

A

No

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20
Q

What is stick force stability

A

Size of force required is greater for further distance from trim position

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21
Q

What is manoeuvre stability

A

Having the right amount of control force to produce a given pitch rate

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22
Q

What are the risks of light manoeuvre stability

A

Overstress

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23
Q

What is stick force gradient

A

The amount of extra stick force that must be applied per unit increase in load factor

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24
Q

Do airliners have a high or low stick force gradient

A

High

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25
How does cg affect stick force gradient
Bigger if cg is forward
26
How does aerodynamic damping affect stick force gradient
More aerodynamic damping at low level = more stickforce required
27
How does aerodynamic damping work
During manoeuvre = reduces effectiveness of tailplane
28
How does being stick free of stick fixed affect the manoeuvre point
Stick fixed = manoeuvre point further back
29
What is the manoeuvre point
The neutral point adjusted for aerodynamic damping (only during the actual manoeuvre) Always aft of neutral point
30
Is the aircraft more or less stable during a manoeuvre
More stable due to damping
31
Can a aircraft be dynamically stable and statically unstable
No for dynamic stability it must be statically stable
32
How do you work out the degree of dynamic stability
Time taken for oscillations to reduce by half
33
What are short period oscillations
Little variation in height or airspeed Large variations in AOA and load factor
34
What is pilot induced oscillations
Pilot trying to correct for short period oscillations but being behind the aircraft and making it worse
35
What is long period oscillations (phugoid)
Little change of AOA or load factor Large variations in height and airspeed
36
How does altitude affect dynamic and static stability
Altitude decreases static and dynamic stability
37
For directional stability what does a positive gradient mean
Positive directional stability
38
What will a aircraft with positive directional stability do
Yaw into the direction of sideslip
39
What is the biggest contributing factor to directional stability
Fin
40
When will the directional stability yawing moment be stronger
Cg further forward Fin is larger Higher IAS Size of side slip angle
41
How does the shape of the fin affect cl and AOA
Straight fin with high aspect ratio = Higher lower AOA and higher Cl
42
What does a dorsal fin do
Increases directional stability Greater sweepback Lower aspect ratio
43
What does a ventral fin do
Increase directional stability
44
What do strakes do
In slow flight rear of aircraft dips into air = creates ventral fin
45
How does sweep back affect directional stability
One wing is more straight on to airflow = more lift (but more drag) therefor yaws towards raf = more stable
46
What does a fuselage do to stability
Destabilises
47
What does weak lateral stability mean
Slow to recover from wing drop
48
What will happen if you have positive lateral stability during a sideslip
Roll in opposite direction of sideslip
49
What gradient does positive lateral stability have
Negative gradient
50
What affect does a dihedral wing have on lateral stability
Increases it
51
What effect does sweepback have on lateral stability
More stable
52
What effect does High wing have on lateral stability
More stable Centre of pressure moves slightly down the downgoing wing creating a moment
53
What affect does High keel surface have on lateral stability
More stable
54
What is spiral instability
When directional stability is strong Lateral stability is weak
55
What is a Dutch roll
Strong lateral stability Weak directional stability Wing drop = wings level (however more drag with extra lift = yaw in direction of wing drop)
56
What does a aircraft that suffers from Dutch roll require
Yaw damper which inputs rudder to prevent yaw
57
Can you fly with an inoperative yaw damper
No
58
How does altitude affect dynamic stability
Reduces with altitude
59
For a canard where must the AC and neutral point me
Forward or the cg
60
What must you remember when calculating stick force per G
To take of 1G for normal gravity