Ch. 2, 3, & 4 Aerodynamics; Rotor Blade; Helicopter Basics Flashcards

1
Q

What are 3 characteristics of an airfoil?

A
  1. Rounded leading edge: ensures smooth flow
  2. Sharp trailing edge: keeps wake behind airfoil small
  3. Specific shaping: reduces turbulence & separation of the layer of air immediately around the surface of the wing (this layer is aka boundary layer)
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2
Q

Resultants are two _____ combined.

A

Vectors

Vectors have both a magnitude (size) & direction

Ex. resultant airflow, resultant relative wind

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3
Q

What is induced velocity?

A

The speed of air being pushed down by the rotor

Don’t confuse this with induced flow.

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4
Q

Define induced flow

A

The mass of air accelerated downwards by the rotor.

Aka downwash

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5
Q

Induced flow is at its greatest during what condition?

A

At a hover with no wind.

This is because there is no horizontal air flow affecting the rotor disc.

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6
Q

Induced flow _____ (increases/decreases) as the AOA of the rotor blades increases.

A

Increases

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7
Q

Resultant airflow is made up of what?

A

The horizontal component from blade rotation & vertical component from induced velocity.

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8
Q

When the AOA becomes too high, about _____ to _____ degrees for most airfoils, the wing produces less useful lift because the airflow has separated from flowing smoothly over the top surface of the airfoil.

A

14-15 degrees

The airfoil is said to be stalled & the airflow on the top surface starts to separate away from the skin of the wing.

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9
Q

What is coefficient of lift?

A

A measure of the amount of lift a particular airfoil shape will produce.

As the airflow meets the segment at steeper & steeper angles, the blade segment produces more & more lift until it reaches the stall AOA. Lift produced decreases rapidly beyond the stall AOA.

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10
Q

What is the spar on a rotor blade?

A

The main longitudinal bean of an airfoil.

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11
Q

Many helicopters’ rotor blades are attached to the hub at a small positive angle. What is this called?

A

Pre-coning

This is built into the rotor hub to reduce stress on the blades & the hub

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12
Q

The _____ degree position on the blade has the minimum blade pitch angle and AOA.

A

90 degrees

Aka advancing side and it’s descending towards the lowest position at the front-“falling down through air”

The blade on the retreating side (270 degrees) is at a very high pitch angle & AOA & is climbing towards the highest position at the back of the disk.

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13
Q

As the blade flaps up & down, the blade _____ moves closer to & further away from the center of the blade.

A

Center of gravity

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14
Q

The _____ requires the blade to speed up as the CG moves towards the center of the hub & slow down as it moves out.

A

Law of Conservation of Angular Momentum

The momentum of the rotating blades can’t change so the velocity has to change to compensate for the change in location of the mass.

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15
Q

What function does the swashplate serve?

A

Transmits the commands of the pilot’s inputs to the rotor blades.

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16
Q

The swashplate has 2 main parts. What are they?

A

Fixed & rotating parts

  • Fixed (aka lower): firmly attached to non-rotating part of airframe
  • Rotating (aka upper): attached to rotor

The driveshaft (or main rotor mast) passes up between the 2 swashplates to drive the hub.