Turning & Stalling Flashcards

1
Q

Centripetal force

A

When turning and keeping on curved effect, this is the force acting on the body forcing it towards the centre of the turn

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2
Q

The horizontal component of lift provides

A

Centripetal force

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3
Q

In a banked turn of 60°, the wings produce a lift force equal to
L = ?
Remember that we need to increase lift in a turn due to loss of lift

A

2W

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4
Q

What happens to the GForce and load factor in a 60 degrees turn

A

G-Force is 2g, the load factor is 2

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5
Q

What is the load factor calculation

A

Lift / weight
OR:
(Wing loading in a manoeuvre) / (wing loading in straight and level)

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6
Q

The more bank degree,

A

The more load factor and g-force felt

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7
Q

An increase of angle of attack will make the induced drag

A

Greater

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8
Q

Since on a turn we lose height, we increase the angle of attack. What it means about airspeed

A

We should increase it

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9
Q

When turning (and increasing the angle of attack to maintain height), what happens to stall speed?

A

Increases

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10
Q

At 60° degrees bank angle the stall speed is increased by

A

41%

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11
Q

“Slipping into the turn”

A

The increase of induced drag on the outer wing (since it’s generating more lift) causes the nose to yaw in the direction opposite of the turn. Need to apply rudder to maintain balance.

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12
Q

Skidding turn

A

When the tail tends to skid onto the outside of the turn,

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13
Q

To maintain a specific radius turn, the more speed

A

The more bank angle required

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14
Q

At constant speed, the greater the bank angle,

A

the tighter the turn

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15
Q

in a constant bank angle, more airspeed will make

A

the radius turn larger

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16
Q

Rate-1 turn meaning

A

180° in 1 minute

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17
Q

Formula to estimate bank angle for a rate-1 turn considering airspeed

A

1/10 * airspeed + 7°

18
Q

How does increased velocity affect static pressure

A

Static pressure decreases

19
Q

What happens to the separation point with higher angle of attacks

A

Comes forward

20
Q

pre-stall buffet (or control buffet)

A

The shaking of the airframe before reaching a stall

21
Q

After exceeding the critical angle, when happens to the center of pressure

A

Moves backwards, therefore lowering the nose

22
Q

How to recover from stall

A

Reduce angle of attack, and incase of low speed, full power

23
Q

Stalling depends directly on

A

Angle of attack and not airspeed

24
Q

If extra lift is needed (more weight) then the stalling speed will be

A

greater

25
Q

Another name for load factor or g-forces is

A

dynamic loading

26
Q

When load factor increases

A

Stalling speed increases

27
Q

If you feel g-forces (load factor increased) that means

A

stall speed increased

28
Q

In a 30° bank turn, stalling speed increases by

A

7%

29
Q

In a 45° bank turn, stalling speed increase by

A

19%

30
Q

In a 60° bank turn, stalling speed increase by

A

41%

31
Q

When lift foce from the wings increases,

A

load factor increases, therefore stalling speed

32
Q

Large wing relative to weight, will make the stall speed

A

decrease

33
Q

In a power-on stall, due to slipstream, the stalling speed

A

is less

34
Q

The slipstream is an airflow with kinetic energy flowing through the aircraft’s by the propoeller, hitting the inner parts of the wing and the complete tailplane. Making the wing at inner ok, and the outer wings to stall. What will happen

A

Rapid roll

35
Q

WIng Washout

A

A lower angle of incidence at the wing-tip than at wing-root. (This means the wing-root will reach stall before the wing-tip)

36
Q

Ice accretion two effect:

A
  • Ice on the upper surface wing will break the streamline flow. Stalling speed will increase
  • Ice will make the aircraft heavier. Stalling speed wil increase
37
Q

Where do ice build more rapidly on the wing

A

Stagnation point

38
Q

Extending flaps will

A

Decrease stall speed

39
Q

Autorotation

A

During stall, the dropping wing becomes furthered stalled and the airplane will roll, sideslip, and nose drop. If no action is taken, the rate of rotatio is increased and now its a spin

40
Q

1c 2

A
41
Q

Load factor calculation formula

A

1/cos(bank angle)

42
Q

Stall speed by load factor formula

A

Vs*root(load factor)