Forces In Descent Flashcards

1
Q

What is the descent angle

A

Angle between ac path through the air and local horizontal
Symbol y (gamma)

Pitch angle + AOA

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2
Q

What is the pitch angle

A

Angle between longitudinal axis and horizontal (shown on attitude indicator)
Pitch angle is less than the descent angle

Given as a negative value

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3
Q

Forces in descent parallel to flight (power on)

A

Drag = Thrust + W Siny

Thrust
Drag
Wsiny

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4
Q

Steeper descent will have a

A

Larger descent angle

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5
Q

Shallowest descent is at

A

VMD

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6
Q

Engine failure you will fly at…

A

Vmd for shallowest descent

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7
Q

Vx

A

Best angle of climb
Steepest climb angle
Operate most efficient at heigh
Slow speed

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8
Q

How do we manage drag

A

Speed and spoilers

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9
Q

Depressurisation what speed should you fly at

A

VMO for most excess drag

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10
Q

Drag in a descent formula

A

T + weight x siny = drag

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11
Q

WSINY =

A

Drag - Thrust
——————
Weight

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12
Q

In a glide descent forward component is what to drag

A

Equal as no thrust

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13
Q

Calculating glide range

A

X lift by the range altitude
Convert ft to nm (6080ft in 1nm)

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14
Q

Gliding with head wind

A

Range reduces

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15
Q

Gliding with tailwind

A

Range increases

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16
Q

Mass impact on glide range

A

Does not affect in still air heavy ac will simply just reach ground quicker in same location

17
Q

Heavy A/C in headwind glide range

A

Will be in air less time therefore less effected so slightly better range than a lighter ac

18
Q

Tailwind and mass

A

Light a/c will have greater range due to being in air longer

19
Q

X2 Factors effecting glide range

A

Flaps - reduce L/D ratio and glide range
Speed - flying faster or slower than vmd

20
Q

Glide endurance speed is

A

Vmp (0.76 vmd)
Useful for gliding over sea
Vmp is the minimum speed for power

21
Q

AOA is always expressed as

A

A positive number of degrees

22
Q

Pitch angle is always

A

Negative

23
Q

In steady power off descent which force drive ac down descent flight path?

A

Weight

24
Q

CDFA Is + advantages

A

Continuous descent final approach

Certain power setting all the way down the descent saves fuel/reduces engine wear and reduces air and noise pollution

25
Q

Glide angle of descent is the ratio of

A

Height lost to the horizontal distance travelled

26
Q

Best glide gradient factors

A

Vmd
Best L/D ratio
CLMAX/CD

27
Q

Formula for descent angle

A

Pitch Angle + AOA
(Always negative) (always positive)

28
Q

How does calculating angle of descent differ from calculating angle of climb

A

Angle of descent uses = siny = drag - thrust
—————-
Weight

Angle of climb uses = siny = thrust - drag
——————
Weight

29
Q

Calculating drag/weight or descent angle in powered off glide

A

Siny = drag
——-
Weight

30
Q

Glide range formula

A

Height x L/D ratio

31
Q

Glide range formula with winds

A

Glide range in still air x ground speed/original TAS

32
Q

Mass on glide range

A

Heavy ac will glide same distance if both fly at Vmd
More induced drag on heavier so has to fly faster vmd so will reach ground quicker

33
Q

Flaps and landing gear on glide range

A

Reduces due to increased drag
Steeper glide path and reduced endurance

34
Q

Headwind will do what to glide range

A

Reduce distance covered over the ground
Does not effect rate of descent

35
Q

Tailwind on glide range

A

Increase our speed
Cover more distance
No effect on endurance

36
Q

Shallowest glide angle is achieved when aircraft is gliding

A

At the speed which equates to best L/D ratio

37
Q

Which force drives ac down the descent angle in power on and off descent?

A

Weight

Driving factor for an aircraft down the descent flight path

38
Q

On a drag polar curve where is VMP to VMD

A

VMD is always below VMP on a CL/CD graph