Helicopter Written Flashcards

1
Q

An _____ is a structure or body which produces a useful reaction to air movement. Airplane wings, helicopter rotor blades, and propellers are airfoils.

A

airfoil

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2
Q

The _____ ______ is an imaginary straight line from the leading edge to the trailing edge of an airfoil.

A

chord line

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3
Q

In aerodynamics, relative wind is the wind felt by an ____________. It is created by the movement of air past an airfoil, by the motion of an airfoil through the air, or by a combination of the two.

A

airfoil

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4
Q

Relative wind is _______ and in the ______ direction to the flight path of the airfoil.

A

paralell

opposite

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5
Q

The _______ __ __________ is the angle at which a wing is attached to the aircraft fuselage.

A

angle of incidence

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6
Q

The _________ ___ __________is the angle between the chord line of the airfoil and the relative wind.

A

angle of attack

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7
Q

An airplane has three axes of rotation: the _____ axis, _________ axis, and the _______ axis.

A

lateral

longitudinal

vertical

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8
Q

The _______ ___ ________ (the imaginary point where all the weight is concentrated) is the point at which an airplane would balance if it were suspended at that point.

A

center of gravity

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9
Q

The four aerodynamic forces which act upon an aircraft are:

A
  1. weight
  2. lift
  3. drag
  4. thrust
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10
Q

As the velocity of a fluid (gas or liquid) increases, its pressure decreases. This is known as__________ ___________.

A

Bernoulli’s Principle

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11
Q

The angle at which a stall occurs is called the_____ __________ ___ __________

A

critical angle of attack

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12
Q

________ __________ is the uncorrected reading obtained from the airspeed indicator.

A

Indicated airspeed

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13
Q

_________ _______ is indicated airspeed corrected for installation and instrument error.

A

Calibrated airspeed

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14
Q

___________ _________ is calibrated airspeed corrected for temperature and pressure variations.

A

True airspeed

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15
Q

_______ ________ is the altitude read on the altimeter after it is set to the current local altimeter setting.

A

Indicated altitude

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16
Q

____ _______ is the height above the surface.

A

Absolute altitude

17
Q

______ ________ is the true height above Mean Sea Level (MSL) normally measured in feet.

A

True altitude

18
Q

________ _________ is the altitude that is indicated whenever the altimeter setting dial (Kohlsman window) is adjusted to 29.92.

A

Pressure altitude

19
Q

________ _______ is the pressure altitude corrected for nonstandard temperature and/or pressure.

A

Density altitude

20
Q

An aircraft may not be operated unless, within the preceding ______ calendar months, it has had an annual inspection and has been approved for return to service

A

twelve

21
Q

In addition, when operating within the lateral boundaries of the surface area of Class B, C, D or E airspace designated for an airport, the ceiling must not be less than _________ feet. If the pilot intends to land, take off, or enter a traffic pattern within such airspace, the ground visibility must be at least _____ miles at that airport.

A

1,000

3