Climbing Flashcards

1
Q

Vx and what is it for a jet and a prop

A

Greatest excess thrust

Vmd for a jet

Vmp for a prop

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2
Q

What happens to Vx when you increase temp

A

For a prop it increases due to increased TAS due to a decrease in density

Same with altitude

Stays the same with a jet for both alt and temp as it is at VMD

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3
Q

Vx for a heavy a/c

A

Faster due to the drag curve moving up and to the right

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4
Q

Vx for a dirty config

A

Will be slower due to the drag curve moving up and to the left

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5
Q

Vx with an engine failure on a jet

A

Slower due to the drag curve moving up and to the left

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6
Q

The effect of an engine failure on climb gradient

A

Reduce it to a quarter

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7
Q

Vx with a prop engine failure

A

Drag curve moves the same way as a jet but Vx gets faster to Vxse

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8
Q

Second segment

A

Engine failure

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9
Q

Effect of wind on flight path angle

A

Increases with a headwind

Decreases with a tailwind

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10
Q

Reducing climb angle

A

Anything which requires acceleration as it requires excess thrust

Turning, the need to increase speed etc

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11
Q

Advantages of using best rate of climb

A

Climb quicker, spend longer in the cruise

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12
Q

Roc formula

A

Roc = angle of climb x speed (TAS)

Roc = Pa - Pr/ W (excess power available)

Roc = g% x TAS

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13
Q

G% formula

A

T-D/w x 100

G% = roc/TAS

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14
Q

Vy

A

Speed for best rate of climb - Max roc

Difference between power required and power available is greatest

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15
Q

Service ceiling

A

Point at which the roc reduces to a specific value

100 fpm for a prop
500 fpm for a jet

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16
Q

Absolute ceiling

A

Height at which the a/c cant climb anymore

Vx is smaller than or equal to Vy

17
Q

Aerodynamic ceiling

A

Coffin corner

18
Q

Certified ceiling

A

The ceiling at which the a/c is certified to fly

19
Q

Factors effecting roc

A

Increasing a/c mass as pr = drag x TAS and induced drag increases

Flaps decrease all vspeeds

Increasing altitude - Tas increases so Pr increases and the curve moves along its own tangent - Vy increases

20
Q

Effect of alt on roc and Vy

A

Excess power and roc reduce

Vy as a CAS reduce

Vy as a TAS increases

21
Q

Effect on temp with roc and Vy

A

On hotter days TAS increases so Vy increases

Roc reduces

22
Q

Effect of engine failure on roc and VY

A

Everything will reduce apart from vx with a prop

23
Q

The effect of wind on roc and Vy

A

Has no effect

24
Q

Effect of acceleration and turning on roc and Vy

A

Reduces roc and angle of climb due to the reduced excess thrust

25
Q

Angle and gradient of climb depends on

A

Excess thrust divided by weight

26
Q

Power formula

A

F x speed (TAS)