Climbing & Decsending Flashcards

1
Q

For a steady climb, the thrust must be efficient to overcome

A
  • Drag
  • Help lift the weight of the airplane at a vertical speed (rate of climb)
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2
Q

In a climb, the lift force is greater / less than weight?

A

Less!

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3
Q

In a climb, thrust is greter /less then drag?

A

Greater! and this help compensate for the reduced lift force

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4
Q

The higher the weight the ___ climb performance

A

The less climb performance

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5
Q

Angle of climb different name

A

Climb gradient

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6
Q

Angle of climb depends on

A

The excess thrust

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7
Q

Maximum gradient (angle) climb

A

Best used to clear obstacles, gains the greatest height in the shortest horizontal distance

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8
Q

Vx

A

maximum gradient speed. use to clear obstacles fast.

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9
Q

Vy

A

Maximum rate climb speed. Used to reach high altitude as quciky as possible, gains the most height in the shortest time.

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10
Q

Maximum rate climb

A

Gains the most height in the shortest time

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11
Q

When weight is increased, the climb performance is

A

decreased

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12
Q

When temparatue increases, the air density?

A

Lowers

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13
Q

When temprate increases the climb perforamnce is

A

decreased

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14
Q

When altitude increases (so does the air density lowers) the climb perforamnce is

A

decreased

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15
Q

Ceiling

A

The altitude at which steady climb perforamnce falls close to zero

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16
Q

Service ceiling

A

When the rate of climb of a steady climb has fallen to 100ft /min

17
Q

Absolute ceiling

A

When the rate of climb is 0

18
Q

Headwind / tailwind effect on climb OVER THE GROUND

A

Headwind will increase climb. Tailwind will decrease

19
Q

Does wind affect rate of climb not over the ground?

A

no

20
Q

Overshoot effect (during windshear) (an increase of headwing component)

A

The climb perforamce will increase

21
Q

Conditions for overshoot effect

A

Flying into an increasing headwind
A decreasing tailwind
Into an updraft

22
Q

Conditions for undershoot (climb perforemce decreased)

A

A decreasing headwind
An increasing tailwind
Into a downdraft

23
Q

The four forces in STEADY STRAIGHT CLIMB:
1. Lift equals weight and thrust equals drag
2. Lift equals weight and thrust is greater than drag
3. Thrust is greater than drag and lift is greater than weight
4. Thrust is greater than drag and lift is less than weight

A

4

24
Q

The angle of climb depends upon:
1. Excess lift and weight
2. Excess thrust and weight
3. Excess thrust and minimum drag

A

3

25
Q

What is Vx?
1. The maximum gradient of climb, giving the greatest height in the shortest time
2. The maximum gradient of climb, giving the greatest in the shortest horizontal distance

A

2

26
Q

When Vx is used, what shoudl the pilot take into account

A

High power settings means poor engine cooling

27
Q

In a glide with no thrust, which force is balancing the drag?

A

Weight. (see page 143)

28
Q

During a glide, if L/D is high

A

Shallow glide path. Will gllide a long way

29
Q

During a glide, if L/D is low

A

Steeper glide path, will glide a short way

30
Q

Flying too slow / too fast during a glide will

A

Make you glide a shorter way

31
Q

Best L/D ratio glide is done by

A

maintaing the airspeed given by the designer (therefore, speed affects angle of attack)

32
Q

Flaps will (glide)

A

steepen the glide

33
Q

How does lower weight affect glide

A

The glide angle will be the same, the glide airpseed will be less
Glide angle will be the same for all weights!!

34
Q

Glide with tailwind / headwind

A

With headwind, shorther distance is covered,
With tailwind, greater distance can be glided

35
Q

If the L/D ratio is 5:1, and you’re 1nm above (6000 ft) how much ground distance will you glide?

A

5 nm

36
Q

6000ft (1nm) above ground, L/D is 9:1. How much distance will be glide

A

9nm

37
Q

The forces acting on a glide are

A

Lift, weight, and drag.
Take note of the weight traingle assisting in maintaing the glide

38
Q

Headwind / tailwind of a glide will affect the distance over the ground. How it will affect the distance over the air mass

A

Nothing

39
Q

In a steady glide, drag is balanced by

A

a component of weight