Straight and Level Flashcards

1
Q

How to remember the usual design of thrust-drag couple being nose-up?

A

If engine fails (thrust is lost), the aircraft will pitch nose-down

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2
Q

In aerodynamics, TAS determines the…

A

Distance travelled through the air

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3
Q

In aerodynamics, IAS determines the…

A

Aerodynamic effects

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4
Q

Formula for practical relationship of forces in straight and level flight

A

Power + Attitude = Performance

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5
Q

On a drag (or thrust required) curve, high thrust is required at which points on the graph?

A

At low speeds (and high AoA) and high speeds (and low AoA)

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6
Q

Maximum endurance speed is

A

The TAS where power is minimum

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6
Q

Maximum range speed is

A

The TAS at which drag is least and L/D ratio is greatest

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6
Q

Maximum endurance speed can be thought of as the speed where what practical measurement is lowest?

A

Fuel flow

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7
Q

TAS at which power (and fuel flow) is minimum is?

A

Maximum endurance speed

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8
Q

Maximum range speed is concerned with what whilst max endurance speed is concerned with what?

A

Greatest Lift/Drag Ratio
Lowest Power

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9
Q

What is speed stable?

A

A higher speed range where minor speed fluctuations are corrected without pilot input

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10
Q

A higher speed range where minor speed fluctuations are corrected without pilot input is known as?

A

Speed stable

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11
Q

If speed stable, an increase of airspeed will mean…

A

Total drag will increase (due to parasite drag)
Drag increase not balanced by constant thrust
Aircraft slows down

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12
Q

If speed stable, a decrease of airspeed will mean…

A

Total drag will decrease (due to parasite drag decrease)
Thrust exceeds drag
Aircraft speeds up

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13
Q

The lower and higher speed range is normally divided by what?

A

Minimum drag speed

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14
Q

In the lower speed range, a decrease in airspeed will mean..

A

Total drag will increase (due to induced drag increasing)
Drag still exceeds thrust
Aircraft continues to slow down

15
Q

In the lower speed range, an increase in airspeed will mean…

A

Total drag will decrease (due to induced drag decreasing)
Thrust still exceeds drag
Aircraft continues to speed up

16
Q

Higher speed range stability is determined by which drag?

A

Parasite drag

17
Q

Lower speed range stability is determined by which drag?

A

Induced drag

18
Q

If rho decreases as altitude increases, how is Lift maintained?

A

V must increase

19
Q

In-flight, how can you ensure V will increase as Rho decreases to maintain constant lift?

A

IAS will remain the same (and TAS correspondingly increases)