ARMY AVIATION INFO Flashcards

1
Q

What is the typical structure of a helicopter (body of the craft) called?

A

The Fuselage

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2
Q

Why does a helicopter need a main rotor?

A

To generate thrust

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3
Q

What is the purpose of a tail rotor?

A

To counteract torque

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4
Q

Why does a single rotor helicopter need a tail rotor?

A

To balance out the effects of torque

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5
Q

On U.S model crafts, in what direction do the rotor blades conventionally spin?

A

Counter-Clockwise

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6
Q

The rotor blades usually spin counter-clockwise in which countries?

A

The U.S.A, U.K, and Germany

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7
Q

True or False: In a single main rotor helicopter, some of the power is used to counteract torque, rather than being used solely for lift.

A

True

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8
Q

True or False: In a tandem rotor helicopter, some of the power is used to counteract torque, rather than being used solely for lift.

A

False.

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9
Q

How many main rotors does a tandem rotor helicopter have?

A

Two

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10
Q

True of False: A tandem rotor helicopter has a secondary/tail rotor.

A

False

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11
Q

What is an advantage of the tandem rotor helicopter, in terms of torque and energy usage?

A

Each blade rotates counter to the other, meaning that torque is automatically offset.

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12
Q

Is the Chinook one of the fastest aircraft in existence? If so, how?

A

Yes. Because of its tandem rotors, all of the power from the Chinook’s engine can be used in lift.

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13
Q

On a Coaxial Rotor Helicopter, in which direction do the blades spin?

A

The two blades spin in opposite directions

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14
Q

How are the blades displayed on a Coaxial Rotor Helicopter?

A

One blade sits on top of the other, mounted to the same mast.

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15
Q

What is one thing that is reduced by a coaxial rotor?

A

Payload

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16
Q

What advantage does an aircraft have by reducing payload?

A

By reducing payload, you are allowed to carry greater cargo and have a higher passenger capacity.

17
Q

What are four aerodynamic forces?

A
  • Thrust
  • Drag
  • Weight
  • Lift
18
Q

How is thrust transferred into motion?

A

By the use of the aircrafts mast and rotors

19
Q

What part of the aircraft creates thrust?

A

The aircrafts engine.

20
Q

What is drag?

A

A disruption in the flow of air due to the objects shape and size.

21
Q

What other aerodynamic force does drag act against?

22
Q

Name four different types of drag.

A
  • Profile Drag
  • Induced Drag
  • Parasite Drag
  • Total Drag
23
Q

Define Profile drag

A

Frictional resistance of a helicopters blades passing through the air.

24
Q

What are two forms of profile drag?

A

Form Drag and Skin Drag

25
Which form of drag is being applied when there is an increase in drag due to an increase of speed of the helicopter?
Form drag
26
The roughness of a rotors blade surface can increase the drag on a aircraft. Which form of drag is this?
Skin drag
27
Which form of drag is caused by the airflow circulation around the blades?
Induced Drag
28
What is parasite drag? Name a few examples.
Any external components to the aircraft. For example, landing gear, doors, or cowlings.
29
When this is at its lowest value, the maximum endurance, and best rate of climb is achieved. What is it?
Total drag.
30
What is the downward force which acts through the center of gravity on the helicopter?
Weight
31
Can a helicopter increase its weight mid-flight?
Yes.
32
Given an aircraft is banking or experiencing severe gusts. What force is applied to the aircraft? What happens as a result?
G force is applied to the aircraft, resulting in an increase of the aircraft's weight.
33
What is the upward force created by the spinning of the helicopters blades, allowing air to pass over them?
Lift
34
What is the term for a helicopter blades direction, relative to the air?
Angle of Attack
35
How can the pilot change his/her Angle of Attack?
By moving the cyclic and collective
36
What are some non-user factors that could impact your Angle of Attack?
- Blade flapping - Blade flexing - turbulent conditions
37
Is the Angle of Attack a mechanical or aerodynamic angle?
Aerodynamic
38
Is the Angle of Incidence a mechanical or aerodynamic angle?
Mechanical
39
What is the intersection of the chord line with the plane of rotation?
The Angle of Incidence OR The blade pitch angle