Lesson 4 Turns, Loads, and Autos Flashcards

1
Q

What is the vertical component of lift?

A

Lift acting upward and opposing weight.

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2
Q

What is the horizontal component of lift?

A

Lift acting horizontally and opposing inertia (centrifugal force).

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3
Q

Define Centrifugal Force.

A

The apparent force that an object moving along a circular path exerts on the body constraining the object, acting outwardly away from the center of rotation.

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4
Q

Define Centripetal Force.

A

The force that attracts a body toward its axis of rotation, opposite to centrifugal force.

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5
Q

What happens to the resultant lift in turning flight?

A

It acts more horizontally, causing the helicopter to bank.

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6
Q

What is Load Factor?

A

The ratio of a specified load weight to the total weight of the aircraft.

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7
Q

How does the angle of bank affect the total lift force?

A

As the angle of bank increases, total lift force tilts more toward the horizontal.

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8
Q

What is the relationship between angle of bank and rate of turn?

A

The rate of turn increases as angle of bank increases.

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9
Q

How does load factor behave in straight and level flight?

A

The load factor is 1G because there is no bank angle.

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10
Q

What happens to load factor during turns?

A

It varies depending on the bank angle; steeper bank angles result in greater load factors.

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11
Q

What is the effect of turbulence on load factor?

A

Increases and decreases in G forces may occur, affecting load factor.

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12
Q

What is autorotation?

A

The condition of flight where the main rotor is driven only by aerodynamic forces without engine power.

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13
Q

What occurs when the engine fails in flight?

A

The freewheeling unit disengages the engine from the main rotor, allowing the rotor to spin freely.

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14
Q

What direction does airflow switch to during autorotation?

A

From horizontal to more vertical as the helicopter descends.

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15
Q

What is the critical factor for maintaining rotor RPM during autorotation?

A

Use of the collective for rotor RPM control.

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16
Q

What happens to rotor RPM in a turn?

A

Increases in load factor and centrifugal force will increase descent rate and airflow through the rotors.

17
Q

What is the minimum autorotational speed?

18
Q

What is the minimum rate of descent speed?

19
Q

What is the maximum glide distance speed?

A

75 KIAS at 90% RPM.

20
Q

What is the ‘Torque Effect’ in autorotation?

A

The aircraft will yaw to the left dramatically when power is lost.

21
Q

What is the ‘Translating Tendency’ when power is lost?

A

The helicopter moves left laterally due to reduced tail rotor thrust.

22
Q

What is the Law of Conservation of Energy?

A

Energy cannot be created or destroyed, only transferred from one form to another.

23
Q

What types of energy are stored during flight?

A
  • Potential Energy (Altitude) * Kinetic Energy (Airspeed) * Inertia (Rotor RPM)
24
Q

Why do we fly around high and fast?

A

To manage energy effectively for autorotation.