Aerodynamic Forces Flashcards

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1
Q

Lift on a wing is most properly defined as the…

A

…force acting perpendicular to the relative wind.

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2
Q

Bags weighing 90 lbs are placed in a normal category airplane’s baggage compartment which is placarded at 100 lbs. if the airplane is subjected to 3.5G positive load factor, the total load factor of the baggage is…

A

315 lbs and would not be excessive

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3
Q

Why is it necessary to increase back elevator pressure to maintain altitude during a turn?
To compensate for the…

A

…loss of the vertical component of lift.

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4
Q

Which airspeed would a pilot be unable to identify by the color coding of an airspeed indicator?

A

Maneuvering speed

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5
Q

Why should speeds above Vne be avoided?

A

Design limit load factors may be exceeded if gusts are encountered

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6
Q

A propeller rotating clockwise as seen from the rear creates a spiraling slipstream. The spiraling slipstream along with torque effect tends to rotate thenairplane to the…

A

Left around the vertical axis and left around the longitudinal axis

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7
Q

If an aircraft with a gross weight of 2000 lbs was subjected to a 60 deg constant altitude bank, the total load factor would be …

A

4000 lbs

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8
Q

In theory, if the airspeed of an airkane is doubled while in level flight, parasitic drag will become…

A

Four times greater

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9
Q

Max structural crushing speed is the max speed the aircraft can operated during…

A

Normal operations

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10
Q

The need to slow an airplane below Va is brought about by the following weather phenomenon…

A

Turbulence which causes an increase in stall speed

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11
Q

The ratio between the total airload imposed on the wing and the gross weight of the airplane in flight is known as…

A

Load factor and directly affects stall speed

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12
Q

A ilit is entering an area where significant clear air turbulence has been reported. Which action is appropriate upon reaching the first ripple

A

Adjust airspeed to that recommended for rough air

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13
Q

Name the four fundamentals involved in maneuvering an aircraft

A

Straight and level flight, turns climbs and descents

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14
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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15
Q

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

A

Flightpath

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16
Q

What increase in load factor would taken place if the angle of bank were increased from 60 to 80

A

4Gs

17
Q

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

A

Decrease the rate of turn resulting in change in load factor

18
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

19
Q

At an airspeed represented by point B, in steady flight, the pilot can expect to obtain the airplane’s maximum…
(The figure depicts a drag vs velocity chart. Induced drag, parasite drag and total drag are drawn on the chart. Point B is the intersection of the induced and parasite drag lines)

A

Glide range

20
Q

If severe turbulence is encountered during flight, the pilot should reduce the airspeed to…

A

Design-maneuvering speed

21
Q

While holding the angle of bank constant in a level turn, if the rate of turn is varied the load factor would…

A

Remain constant regardless of the air density and the resultant lift vector

22
Q

Airplane wing loading during a level coordinated turn in smooth air depends on the…

A

Angle of bank

23
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

24
Q

Which statement is true, regarding the opposing forces acting on an airplane in steady state level flight?

A

These forces are equal

25
Q

By changing the angle of attack of a wing, the pilot can control the airplane’s…

A

Lift, airspeed and drag

26
Q

A aircraft wing is designed to produce lift resulting from a difference in the…

A

Higher air pressure below the wing’s surface and lower pressure air above the wing’s surface

27
Q

If the airspeed is increased from 90 knots to135 knots during a level 60 deg banked turn, the load factor will…

A

Remain the same but the radius of turn will increase

28
Q

During the transition from straight and level flight to a climb, the angle of attack is increased and lift…

A

Is momentarily increased

29
Q

Which is true regarding the force of lift in steady, unaccelerated flight?
(Regarding the relationship between airspeed and angle of attack)

A

There is a corresponding indicated airspeed required for every angle of attack to generate sufficient lift to maintain altitude

30
Q

If airspeed is increased during a level turn, at action would be necessary to maintain altitude? The angle of attack…

A

Must be decreased or angle of bank increased

31
Q

Which statement is true relative to changing angle of attack?
( as it relates to drag)

A

An increase in angle of attack will increase drag

32
Q

Lift on a wing is most properly defined as the…

A

Force acting perpendicular to the relative wind

33
Q

In theory, if the angle if attack and other factors remain constant and the airspeed is doubled, the lift produced at the higher speed will be…

A

Four times greater than at the lower speed