CADH Practice Cards 5 Flashcards

Random questions/statements for exam preparation

1
Q

Flapping to equality means…

A

Allowing the blades to flap of thier own accord, increasing and decreasing pitch angles by the adjustment of induced flow to increase and decrease lift respectively.

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2
Q

The inflow angle is defined as …

A

the angle between the relative airflow and the rotational flow

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3
Q

Refer to diagram

THe diagram shows a rotor blade in …

A

the autorotative drive region

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4
Q

Dissymmetry of lift is over come by …

A

allowing blades to flap

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5
Q

Rotational airflow is..

A

Airflow due to the actual rotation of the blade, parallel to the plane of rotation.

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6
Q

Refer to diagram

Lift is represented by the vector …

A

D

The diagram is of the autorotative drag region

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7
Q

Ground resonance may be caused by …

A

a geometric imbalance of a fully articulated rotor system

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8
Q

The relative wind angle that will produce weathercocking is….

A

180 degrees.

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9
Q

Refer to vector diagram -

Induced flow is represended by the letter …

Vector Diagram in powered flight
A

G

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10
Q

The mean camber line of an aerofoil is a line …

A

drawn halfway between the upper and lower surfaces of an aerofoil, starting at the centre of curvature of the leading edge and ending at the centre of the training edge

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11
Q

The total reaction force is defined as …

A

the resultant of the pressure forces acting on an aerofoil

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12
Q

In a hover left turn, the tail rotor …

A

pitch increases

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13
Q

Raising the collective will….

A

Collectivly change the pitch (and equal amount) relative to the rotor hub.

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14
Q

Aircraft designers can incorporate a feature into the blade design to prolong the effect of comressibility, this is known as…

A

Swept back tips

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15
Q

Lift is defined as …

A

the component of total reaction acting perpendicular to the relative airflow

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16
Q

Three benifits of a flare are…

A

Decrease ROD, decrease FWD airspeed and Increase RRPM

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17
Q

Refer to diagram

Drag is represented by the vector …

A

G

The diagram is of the autorotative drag region

18
Q

In overcoming dissymmetry of lift, the angle of attack on the advancing blade …

19
Q

The relative airflow presenting to an aerofoil is defined as …

A

the single airflow presented to an aerofoil after adding up all the smaller airflow components

20
Q

In cruise you experience low rotor RPM and low manifold pressure. To remedy this you would …

A

increase throttle

21
Q

During autorotation the pilot controls the rotor RPM by using …

A

the collective

22
Q

What does the swashplate do …

A

applies cyclic and collective control to the main rotor

23
Q

Hovering in ground effect (HIGE) would be most useful when…

A

hovering at high density altitudes with high AUW

Ref: Principles of Helicopter Flight, Chapter 11, pg. 81

24
Q

A one-per-rev vertical vibration can be caused by a…

A

Out of track main rotor.

Principles of Helicopter Flight, Chapter 20

25
Q

Refer to vector diagram -

Lift is represented by the letter …

Vector diagram for powered flight
26
Q

Two indicators of a sudden increase in headwind during approach to land would be….

A

an increase in indicated airspeed and a decrease in rate of descent.

27
Q

Drag is defined as …

A

the component of total reaction acting parallel to the relative airflow

28
Q

When the angle of attack increases, drag increases and lift decreases.
True or False?

29
Q

During forwards autorotation, the pattern of driving and propeller region distribution over the disc is …

A

moved toward the retreating side

30
Q

Induced drag at the blade tip is know as…..

31
Q

In relation to aerodynamics, high air density can….

A

increase engine power, increase thrust and increase lift.

32
Q

The plane of rotation is defined as …

A

the plane passing through the rotor hub parallel to the plane in which the blades rotate

33
Q

Assuming all other factors are equal, a decrease in airspeed will require an increase in angle of attack to stay in straight and level flight.
True or False?

34
Q

The effect that a headwind will have on the ROC is…

A

none, the ROC remains unchanged, however the angle at which the aircraft will climb will be effected.

35
Q

Angle of attack and airspeed are inherently linked, so in a straight and level flight we can assume…..

A

that as airspeed increases, angle of attack decreases.

36
Q

A standard rate turn can be completed in…

A

2 minutes.

37
Q

if you double the spped in a turn for a given bank angle, the radius will….

A

quadruple.

38
Q

Ground effect is most noticeable…

A

Just above the ground

39
Q

Load factor equals….

A

Lift / Weight

40
Q

The tip path plane is defined as …

A

the plane passing through the blade tips parallel to the plane in which the blades rotate