Aerodynamics and Aircraft Flashcards

1
Q

Lateral axis is

A

Along the wings

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2
Q

Useful Load

A

total weight of passengers, fuel, baggage and pilots

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3
Q

Basic Empty Weight

A

Standard Empty Weight plus optional equipment (GPS, ect.)

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4
Q

Standard Empty Weight

A

airframe plus engine, oil, hydro, unusable fuel

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5
Q

Single engine failure on a multiengine plane reduces climb by…

A

80%

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6
Q

Banking toward the operative prop…

A

increases climb performance

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7
Q

The critical engine on most light multiengine planes with clockwise rotating props is the…

A

left engine, because of p-factor of the right prop

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8
Q

How does a cruise propeller differ from a climb propeller during cruise operations?

A

A cruise prop has a higher pitch therefore more drag. More drag results in lower RPM and less hp capability. Decreases performance during takeoff and climb but increases efficiency during cruise flight.

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9
Q

Phugoid Oscillation

A

A slow rhythmic change in pitch and altitude, accompanied by changes in airspeed as aircraft climbs and descends.

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10
Q

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

A

one fourth as much

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11
Q

Profile drag =

A

Skin friction

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12
Q

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

A

four times greater

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13
Q

While maintaining a constant angle of bank and altitude in a coordinated turn, an increase in airspeed will..

A

decrease the rate of turn resulting in no change of load factor

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14
Q

Why does increasing the speed also increase lift?

A

The increased impact of the relative wind on an airfoils lower surface creates a greater amount of air being deflected downward

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15
Q

The load factor in a level coordinated turn with 60 degrees of bank is

A

2 Gs

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16
Q

What effect does uphill runway slope have on takeoff performance

A

increases takeoff distance

17
Q

Lift on a wing is most properly defined as the…

A

force acting perpendicular to the relative wind.

18
Q

The angle of attack of a wing directly controls the…

A

distribution of pressure acting on the wing.

19
Q

Lift Equation

A

Lift= CL x P x V squared x S

20
Q

A glide slope is being flown. What characteristics should be observed when a headwind shears to a constant tailwind?

A

Pitch attitude- decreases, Required thrust- increases then decreases, vertical speed increases, IAS decreases then increases to approach speed

21
Q

To establish a climb after takeoff in a plane with a constant speed prop. the output of the engine is reduced to climb power by decreasing manifold pressure and…

A

decreasing RPM by increasing prop blade angle.

22
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.

23
Q

If necessary to take off from a slushy runway, the freezing of landing gear mechanisms can be minimized by…

A

recycling the gear