Lesson 3 Aerodynamics of Flight Part 2 Flashcards

1
Q

What are the three regions of the rotor?

A

Stalled (Large force against rotation, rotor drag 25%), Driving (Good, produced force in the direction of the rotation 45-75%), Driven (Slight force against rotation 30%)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Blade forces move to which side of the rotor in forward flight? Why?

A

The retreating side because of dissymmetry of lift.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

What happens to the driving region when you raise or lower the collective in an autorotation?

A

When you raise the collective, less driving, more drag.
Lower collective, more driving, less drag

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

Explain what happens to the RPM in an autorotation when you:
1) raise collective
2) lower collective
3) forward cyclic
4) rear cyclic

A

1) RPM decreases
2) RPM increases
3) RPM decreases
4) RPM increases

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

What is the shaded area of the high/velocity diagram?

A

This is the area that may not allow for a safe autorotation, given an engine failure.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

When in an autorotation and turning, you must do what to the collective? Why?

A

Raise the collective slightly, in order to prevent a rotor overspeed.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

Describe an autorotative flair (2 items)

A
  • Aft cyclic to tilt the disc back against the wind
  • This speeds the rotor system RPM up (storing energy in the rotor system to cushion landing
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

In the autorotation, how do updrafts and downdrafts affect the rotor RPM?

A

Updrafts, increase rotor RPM
Downdrafts, decrease rotor RPM

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

What is effective translational lift (4 items)

A
  • Occurs between 16-24 knots
  • Helicopter moves out of wing tip vortices
  • Tail rotor becomes more efficient
  • Helicopter climbs and yaws left
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

What is transverse flow (5 items)

A
  • Front of rotor is in undisturbed horizontal air
  • Rear of rotor is in disturbed vertical air
  • 10-20 knots
  • Helicopter shudders due to unequal induced drag
  • Nose climbs, rolls right (gyroscopic precession), yaws left (tail rotor)
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

What is translational lift

A
  • Additional lift occurs
  • Induced flow is more horizontal
  • Angle of attack increases
  • Induced drag decreases
How well did you know this?
1
Not at all
2
3
4
5
Perfectly