Drag Flashcards

1
Q

Parasite Drag is made up of:

A

Skin friction drag.
Form (Pressure) drag.
Interference drag.

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2
Q

Induced Drag

A

Spanwise airflow generates wing tip vortices.

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3
Q

Total Drag

A

Total drag is the sum of Parasite drag and Induced drag.

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4
Q

At low IAS ____ drag is dominant.
At high IAS ____ drag dominates.

A

At low IAS Induced drag is dominant.
At high IAS Parasite drag dominates.

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5
Q

At a constant IAS, ____ has no effect on Total drag, but TAS will increase as density decreases
with increasing ___.

A

At a constant IAS, ALTITUDE has no effect on Total drag, but TAS will increase as density decreases
with increasing ALTITUDE.

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6
Q

By changing the angle of attack of a wing, the pilot can control the aeroplane’s:

A

lift, airspeed, and drag.

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7
Q

What is the relationship between induced and parasite drag when the gross weight is increased?

A

Induced drag increases more than parasite drag.

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8
Q

In theory, if the airspeed of an aeroplane is doubled while in level flight, parasite
drag will become:

A

four times greater.

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9
Q

As airspeed decreases in level flight below that speed for maximum lift/drag ratio, total drag of an aeroplane:

A

increases because of increased induced drag.

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10
Q

At the airspeed represented by point B, in steady flight, the
aeroplane will:

A

have its maximum L/D ratio.

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11
Q

On a wing, the force of lift acts perpendicular to, and the force of drag acts parallel to the:

A

flight path.

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12
Q

That portion of the aircraft’s total drag created by the production of lift is called:

A

induced drag, and is greatly affected by changes in airspeed.

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13
Q

The best L/D ratio of an aircraft occurs when parasite drag is:

A

equal to induced drag.

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14
Q

At a given True Airspeed, what effect will increased air density have on the lift and drag of an aircraft?

A

Lift and drag will increase

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15
Q

The best L/D ratio of an aircraft in a given configuration is a value that:

A

remains constant regardless of Indicated Airspeed changes.

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16
Q

The tendency of an aircraft to develop forces which restore it to its original
condition, when disturbed from a condition of steady flight, is known as:

A

stability.

17
Q

If the same angle of attack is maintained in ground effect as when out of ground effect, lift will:

A

increase, and induced drag will decrease.

18
Q

Aspect ratio of a wing is defined as the ratio of the:

A

wingspan to the mean chord.