Aerodynamics 3 Flashcards

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1
Q

what are the nonstandard conditions that a sensitive altimeter can face?

A

mechanical and inherent

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2
Q

Altimeter indication is off more than 75 feet from the surveyed elevation,

A

next step is: instrument repair station

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3
Q

You are flying an aircraft with an auxiliary electric fuel pump When should this pump be used?

A

in accordance with the POH instructions.

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4
Q

Which statement Is true about isogonic lines?

A

lsogonic lines are lines of equal variation.

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5
Q

What is zero fuel weight?

A

the maximum allowable
weight of the airplane and payload, assuming there is
no usable fuel on board.

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6
Q

What is the purpose of zero fuel load?

A

limit load forces on

the wing spars with heavy fuselage loads.

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7
Q

On a fixed pitch propeller, the angle of incidence is a its highest pitch at the ________________________

A

hub of the propeller in order to provide uniform lift across the blade.

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8
Q

Difference between normal airfoil and propeller airfoil

A

The propeller is a rotating airfoil, subject to induced drag, stalls, and other aerodynamic principles that apply to any
airfoil.

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9
Q

wingtip vorticies drift

A

with the wind and at the same speed.

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10
Q

Direction of the vortices

A

outward, upward, and around the wingtips

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11
Q

vortices are

the by product of _______

A

wing lift

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12
Q

how Wingtip vortices move?

A

1) bit less than a wingspan apart,
2) drifting with the wind,
3) at altitudes greater than a wingspan from the ground.

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13
Q

To avoid excessive cylinder head temperature

A

increase airspeed, enrich the mixture, and/or reduce power use the cowl flap

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14
Q

The cruise propeller has increased efficiency foc cruise operations and has a

A

The cruise propeller has a higher pitch, therefore more drag. More drag results in lower rpm and less horsepower capability, which decreases performance during takeoffs and climbs but increases efficiency during cruising flight.

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15
Q

As air speed increases ,parasite drag increases

A

as the square of the airspeed.

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16
Q

Which factor remains constant for stalls?

A

Angle of attack.

17
Q

While accelerating for takeoff, you notice the airspeed Is constant and remains constant for a few seconds. This can be caused by

A

a winds hear to an increasing tailwind.

18
Q

What is wing loading?

A

dividing total weight of an airplane in pounds by the wing area in square feet

19
Q

how does density affect lift and drag? compare 18000 to Sea Level

A

18,000 feet, the density of the air has one-half the density of air at sea level.
In order to maintain its lift at a higher altitude, fly at a greater true airspeed for any given AOA. so Lift and Drag will increase

20
Q

The direct cause of every stall is

A

airflow separating from the surface of the wing.

21
Q

Critical Mach number

A

airflow over any part of the aircraft first reaches

the Mach 1.0

22
Q

Ramp Weight

A

Zero fuel weight plus usable fuel weight.