1: (94) Airplanes and Aerodynamics Flashcards

1
Q

In theory, if the airspeed of an aircraft is cut in half while in level flight, parasite drag will become…

A

one-forth as much

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2
Q

Which is true regarding the forces acting on an aircraft in a steady-state descent? The sum of all…

A

forward forces is equal to the sum of all rearward forces.

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3
Q

Which factor below is the best indication of positive or negative Gs in an aircraft?

A

Change in how heavy you feel in your seat.

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4
Q

One of the main functions of flaps during the approach and landing is to…

A

provide the same amount of lift at a slower airspeed.

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5
Q

If an airplane is loaded to the rear of its CG range, it will tend to be unstable about its…

A

lateral axis

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6
Q

How many feet in statute mile ?

A

5280

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7
Q

Acceleration past critical Mach speed may cause compressibility issues such as…

A

drag increases

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8
Q

What is the critical Mach number ?

A

highest flight speed possible without supersonic flow.

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9
Q

Lift on a wing is most properly defined as the…

A

force acting perpendicular to the relative wind.

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10
Q

The ratio of an airplane’s true airspeed to the speed of sound in the same atmospheric conditions is…

A

Mach number

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11
Q

When a pilot increases the angle of attack on a symmetrical airfoil, the center of pressure will…

A

be unchanged

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12
Q

At the airspeed represented by point A (minimum total drag curve), in steady flight, the airplane will…

A

have its maximum L/D ratio

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13
Q

Which is true regarding the use of flaps during level turns?

A

The raising of the flaps will increase stall speed.

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14
Q

Stall speed is affected by…

A

weight, load factor, and power.

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15
Q

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

A

increases because of increased induced drag.

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16
Q

What performance is characteristic of flight at maximum lift/drag ratio in a propeller-driven airplane? Maximum…

A

range and maximum distance glide.

17
Q

Load factor is the lift generated by the wings of an aircraft at any given time…

A

divided by the total weight of the aircraft

18
Q

If a standard rate turn is maintained, how long would it take to turn 360°?

A

2 min

19
Q

Select the correct statement regarding stall speeds. The airplane will stall…

A

10 knots higher in a power-on, 60° bank, with gear and flaps up, than with gear and flaps down.