H2-2a Airfoil, Airfow (2.8-2-17) Flashcards

2.8 Airfoil 2.9 Airflow, and reactions in the rotor disc, relative wind, rotational relative wind 2-11 Resultative relative wind, induced flow 2-12 Rotor blade angles 2-14 Powered flight, hovering flight 2-15 translating tendency, pendular action 2-16 coning, Coriolis effect, 2-17 gyroscopic precession

1
Q

2-9 give one disadvantage of a non-symmetrical airfoil

A

The center of pressure travel up to 20% of the cord line creating undesired will work on the airfoil structure and greater production cost

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2
Q

2-9 define hub

A

On the mast, the attachment point for the root of the blade and the axis about which blade rotates

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3
Q

2-9 How is the angular position of the main rotor blade measured?

A

From the helicopters longitudinal axis and usually from the nose

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4
Q

2-9 What is the radial position of a segment of a blade?

A

The distance from the hub as a fraction of the total distance

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5
Q

2-9 what is tip-path plane

A

Rotational relative wind. The rotation of rotor blades as a turn about the mast produces rotational relative wind.

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6
Q

The term “rotational” in Rotational Relative Wind refers to the method of..

A

producing relative wind.

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7
Q
A
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8
Q

H.2-10 TAF

A

Total aerodynamic force aka Total Resultant force

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9
Q

2-10 what is induced flow

A

Downwash

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10
Q

2-10 is the blade angle of attack in the aft section of a helicopter greater or smaller than induced flow

A

Smaller

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11
Q

What happens to induced drag in ground effect.

A

the previous aft lifting force is now straight up, removing the induced drag

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12
Q

What is relative wind?

A

the airflow which moves parallel but against the airfoil

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13
Q

What is lifts relationship (angle) to resultant relative wind?

A

Lift acts perpendicular to resultant relative wind.

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14
Q

What is the angle of incidence on a helicopter

A

the angle between the chord line of a main or tail rotor blade and it’s rotor.

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15
Q

2-14 what is the primary means for compensating for dissymmetry of lift?

A

Flapping

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16
Q

H.2-15 The main transmission is mounted at a slight angle to the left. Why?

A

So that the rotor mast has a built-in tilt to oppose the tail rotor thrust

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17
Q

2-15 To which side is the tip path plane tilted in hover

A

Left

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18
Q

2-15 What is inherent slip slide?

A

In forward Flight, the tail rotor continues to push to the right and the helicopter makes a small angle with the wind when the rotors are level and the slip ball is in the middle. See 12-2

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19
Q

2-15 What is translating, tendency or translating drift?

A

Upon lift off, the helicopter will move to the right due to rear rotor anti-torque usage

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20
Q

What is rolling tendency?

A

When the entire helicopter moves to the right and angles upward due to tail rotor anti

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21
Q

What are the three types of rotor systems?

A

Rigid, Semi-Rigid, Fully Articulate

22
Q

List characteristics of a fully articulated rotor system

A

Lead and lag, flap and feather independently

23
Q

This characteristic of a semi rigid rotor system

A

Flap and feather, but do not lead and lag

24
Q

What can a rigid rotor system do

A

Feather only

25
Q

2-16 what are the three major causes of coning?

A

Lift, Weight, centrifugal force

26
Q

conservation of angular momentum

27
Q

What’s another name for Coriolis effect

A

Law of conservation of angular movement

28
Q

What is angular movement

A

The movement of inertia (mass times distance from the center of rotation squared) multiplied by the speed of rotation

29
Q

What are the four things that happen when coning

A

-G loading increases coning
-Blade diameter shrink
-center of gravity shifts inward
-Rotor RPM increases

30
Q

What is CL max

A

Critical angle of attack.
Greatest coefficient of lift than can be produced.

31
Q

What does CL stand for?

A

Coefficient of lift

32
Q

What is Coefficient of lift

A

The coefficient of lift is a dimensionless number that describes the contribution to lift as a result of airfoil shape and angle of attack

33
Q

What is the formula for Lift

A

L = Cl 1/2pV2 (squared) S
Lift = Coefficient of life
x 1/2 True airspeed (Air Density (or ROW) and Freestream Velocity (True airspeed)
x Wing surface area

34
Q

Is it true that a higher AOA produces a lower IAS and vice versa

35
Q

What is VRS

A

Vortex ring State. Dirty air

36
Q

MEA

A

Minimum En Route Altitude (top # above “Low IFR map”) see OROCA

37
Q

MEF

A

Maximum Elevation Figure (big3 small 1 on SAC)

38
Q

MEL

A

Mimimum Equipment list - allowed to be broken and still fly

39
Q

METAR

A

Meterological aerodrome report

40
Q

MFD

A

Multi-Function Display

41
Q

MH

A

Magnetic Heading

42
Q

MIRL

A

Medium Intisity Runway Lighting (US Chart Sup)

43
Q

MOA

A

Military Operations Area

44
Q

MOCA

A

Minimum Obstical Clearance Altitude (Botton * # on “Low IFR” highway map”) see OROCA

45
Q

MRA (reception)
R

A

Minimum Reception Altitude (R in a square at Victor intersections)

46
Q

MSL

A

Mean Sea Level

47
Q

MTOS (obscursion)

A

Mountain obscuration

48
Q

MTR (military)

A

Military Training route (gray lines on SAC. VR (<1500ft AGL with 4 digits. above with 4 digit #) or IR (atc control and >1500ft AGL. 3 digit number). width from 4m to 16. Cross at 90* angle. Contact FSS.

49
Q

MVFR

A

Marginal Visual Flight Rules

50
Q

NAS (national)

A

National Airspace System