10 LP Principles Of Flight Flashcards

1
Q

What is the primary source of lift

A

Pressure differential around an airfoil

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2
Q

What is the result of Bernoulli’s principle

A

Lift

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3
Q

What is a secondary source of lift

A

And upward force generated by air striking the underside of an airfoiland being deflected downwards

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4
Q

What is generated when an upward force of airstrikes the underside of an airfoil

A

The secondary source of lift

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5
Q

The primary source of lift on an airfoil is created by a differential in

A

Pressure

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6
Q

The statement “ the internal pressure of a fluid decreases at the point where the speed of the fluid increases” is a part of

A

Bernoulli’s principle

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7
Q

The direction of airflow produced by an object moving through the air

A

Relative wind

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8
Q

The relative wind for an aircraft in-flight flows in a direction ______ with and ______ to the direction of flight

A

Parallel

Opposite

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9
Q

What determines the direction of relative wind

A

Actual flight path of the aircraft

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10
Q

What are The three principal airfoils that produce lift on an aircraft

A

Wing, horizontal tail surfaces, propeller

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11
Q

What are the three parts of an airfoil

A

Leading edge, trailing edge, chord line

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12
Q

And imaginary straight line drawn from the leading edge to the trailing edge of a cross-section of an airfoil

A

Chord line

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13
Q

The acute angle formed between the cord line of an airfoil and the direction of the air striking the airfoil

A

Angle of attack

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14
Q

The curvature of the airfoil from the leading-edge to the trailing edge

A

The camber

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15
Q

The shape or form of a wing as viewed from above

A

Wing platform

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16
Q

The four forces affecting flight

A

Lift weight thrust drag

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17
Q

Upward force created by an airfoil when it is moved through the air

A

Lift

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18
Q

Downward force which tends to draw all bodies vertically toward the center of the earth

A

Weight

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19
Q

Man-made force that pulls or pushes the aircraft are there

A

Thrust

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20
Q

Rear word acting force which resists the forward movement of that airplane through the air

A

Drag

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21
Q

If Lift is greater than weight

A

Aircraft will climb

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22
Q

If weight is greater than lift

A

The aircraft will descend

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23
Q

More thrust =

A

More drag

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24
Q

Three key properties of the atmosphere that affect air density and aircraft performance

A

Temperature, altitude, water vapor/humidity

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25
As altitude increases the temperature decreases on average
2°C every thousand feet until the air temperature reaches about 67° at 7 miles above earth
26
Is cold air denser than warm air?
Yes
27
A decrease temperature with height
Lapse rate
28
What is the measurement of 29.92 in inches of _____
Inches of mercury
29
Pressure ______ with height
Decreases
30
Lower pressure results in
Less dense air
31
The altitude in the standard atmosphere corresponding to a particular value of air density
Density altitude
32
Higher density altitude indicates
Lower density air, thinner air
33
A device for propelling an aircraft that when rotated, produces by its action on the air, a breast approximately perpendicular to its plane of a rotation
Propeller
34
What are the three different types of propellers
Adjustable pitch, fixed pitch, controllable pitch
35
What are the three axes of rotation on an aircraft
Longitudinal axis, role, lateral axis, pitch, vertical axis, yaw
36
An imaginary straight line through the fuselage nose to tail
Longitudinal axis, roll
37
A line through the wing from wingtip to wingtip
Lateral access, pitch
38
A line through the center of gravity from top to bottom
Vertical axis, yaw
39
What do these control Ailerons Elevator Rudder
Controls roll,- longitudinal moves as the units/controls pitch,- lateral controls yaw- vertical
40
A hinge surface normally mounted on out board trailing edge of the wing
Ailerons
41
The control you control the ______ and _____
Ailerons | Elevator
42
A hinge surface normally located on the rear of a horizontal stabilizer
The elevator
43
The aft of the vertical stabilizer
The rudder
44
How is the rudder controlled
By the rudder pedals on the floor
45
Small, adjustable, hinged surfaces on the trailing edge of the primary control surface
Trim tabs
46
What is the purpose of trim tabs
To lessen the manual pressure on the controls
47
Located in board on the wings trailing edge and are used to increase lift
Flaps
48
The extension of flaps causes an increase in
Drag
49
What does the cyclic and collective control
Cyclic equals tilt, collective equals pitch
50
The state a flight where the main rotor system has been turned by the action of relative wind rather than engine power
Auto rotation
51
When does a stall occur
15-20 degrees | The airfoil reaches a critical angle of attack
52
Three primary causes of stalls
Insufficient airspeed, excessive violence flight maneuvers, severe wind shear
53
Three types of icing
Structural Icing, Pito static system icing, carburetor Icing
54
Changes the shape of the airfoil
Structural Icing
55
What type of icing reduces the fuel/airflow to the engine
Carburetor Icing
56
Name five aircraft system failures
``` Electrical, mechanical, hydraulic, engine, engine fire ```
57
What type of failure? Some instruments, flaps on some aircraft, radios, navigation and transponder equipment, lights
Electrical failure
58
What kind of failure? Landing gear, blown tire, wheel off, panel off, flight controls, windshield
Mechanical failure
59
What kind of failure? Effects landing gear, flaps, brakes on some aircraft
Hydraulic failure
60
What kind of failure? Engine driven vacuum system for instruments, hydraulic power, electrical power, pressurization, forced landing, loss of altitude
Engine failure
61
What type of failure is usually controllable
Engine fire