Lesson 2 Aerodynamics of Flight Part 1 Flashcards

1
Q

Induced Flow

A

The component of air flowing vertically
through the rotor system resulting from the production of lift.

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2
Q

Lift is always ____________ to the chord line

A

Resultant lift

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3
Q

How much of lift can be attributed to Bernoulli’s principle?

A

70%

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4
Q

How much of lift can be attributed to Newton’s third law?

A

30%

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5
Q

Parasite drag

A

The part of total drag created by the form or
shape of helicopter parts. (4x airspeed)

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6
Q

Profile drag

A

Drag incurred from frictional or parasitic resistance of the blades passing through the air. It does not change significantly with the angle of attack of the airfoil section, but it increases moderately as airspeed increases.

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7
Q

Induced drag

A

That part of the total drag that is created by
the production of lift.

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8
Q

The four forces of flight?

A

Lift, weight, thrust, drag

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9
Q

Relative wind

A

Air flow in relation to the direction of the surrounding air.

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10
Q

Translating Tendency

A

The tendency of the single-rotor helicopter to move laterally during hovering flight. Also called tail rotor drift.

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11
Q

______________ is pushed to the left of the tail rotor and __________ is going to the right.

A

Downwash, thrust

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12
Q

If left uncorrected, which way will a helicopter drift because of translating tendency?

A

It will drift to the right. Tail thrust to the right, turns the nose to the right, causing the helicopter to drift to the right.

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13
Q

Pendular action

A

The lateral or longitudinal oscillation of
the fuselage due to its suspension from the rotor system.

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14
Q

What three things cause pendular action?

A

Too late, too long, too strong (control movements)

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15
Q

Coning

A

An upward sweep of rotor blades as a result
of lift and centrifugal force.

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16
Q

What three things cause coning?

A

Think a helicopter at rest (weight)
Think a helicopter with blades spinning on the ground (centrifugal force)
Think a helicopter in the air (lift)

17
Q

Coriolis effect

A

The tendency of a rotor blade to increase or
decrease its velocity in its plane of rotation when the center of mass moves closer to or farther from the axis of rotation.

18
Q

How does an R22 avoid Coriolis effect?

A

It has an underslung rotor. The underslung rotor and the way it moves, keeps the CG of the blade in roughly the same place when the blade flaps up/down.

19
Q

Pitch angle

A

Difference between the chord line and the plane of rotation.