18. Forces acting on an aircraft (straight and level flight) Flashcards

1
Q

The four main forces acting on an aircraft in flight are …….., …….., …….., and ……..

A

Lift; weight; thrust; drag

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2
Q

In straight and level flight at a constant airspeed, the aircraft is in equilibrium, with the weight counteracted by the …….. and the drag counteracted by the ……..

A

Lift; thrust

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3
Q

To accelerate an aircraft in level flight:

a) thrust must exceed drag
b) thrust must equal drag
c) drag must exceed thrust
d) thrust must equal weight

A

A

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4
Q

Complete the following phrase: “power plus attitude equals ……..”

A

Performance

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5
Q

To fly faster but remain in level flight the nose attitude must be progressively (raised / lowered) at the same time as power is applied.

A

Lowered

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6
Q

As airspeed increases in level flight, drag builds up until it is equal to …….. and the forces will return to a new state of equilibrium

A

Thrust

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7
Q

After an increase of speed in level flight, the nose attitude will be (higher / lower) than previously.

A

Lower

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8
Q

To decelerate an aircraft in level flight:

a) thrust must exceed drag
b) thrust must equal drag
c) drag must exceed thrust
d) drag must equal weight

A

C

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9
Q

After a decrease in speed in level flight, the nose attitude will be (higher / lower) than previously

A

Higher

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10
Q

In steady -state flight, the sum of the opposing forces acting on an aircraft (is / is not) zero.

A

Is

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11
Q

What two factors determine the performance of an aircraft?

A

Power and attitude

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12
Q

In flight, the lift/weight and the thrust/drag pitching couples rarely balance out and it is the function of the …….. to provide the necessary stabilizing force

A

Tailplane (or horizontal stabilizer)

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13
Q

The maximum speed possible in straight and level flight occurs when the power …….. is equal to the power ……..

A

Available; required

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14
Q

The minimum speed straight and level is usually when the …….. angle of attack is reached.

A

Stalling

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15
Q

Maximum range in level flight is achieved when the …….. distance is flown for the …….. amount of fuel used.

A

Maximum; minimum (or least)

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16
Q

Maximum endurance will be achieved when the aircraft remains airborne for the greatest amount of …….. for the …….. amount of fuel used.

A

Time; least