Module 2 Theory of flight Flashcards

1
Q

Atmospheric composition or AIR

A

-Nitrogen=78%
-Oxygen=20%
-Argon= 1%
-Carbon dioxide =0.04%
and small amount of other gases

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2
Q

Air is a gas, gases have various properties named them

A
  • Pressure
  • Temperature
  • Mass
  • The volume which contain the gas
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3
Q

Boyle’s law

A

pV=C

If temperature of the gas is held constant(temp), The absolute pressure is inversely proportional to the volume

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4
Q

Charles’ law

A

If the temp increases volume also increases in order to maintained the same constant ( pressure)

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5
Q

Density

A

Mass of an object divided by its volume

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6
Q

What will happen to the density of air when temperature increases?

A

When the temperature of air increases, the density of that air will decrease

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7
Q

International Standard Atmosphere

(Sometimes referred to as Standard Day

A
  • Atmospheric pressure of
    29. 92 In Hg (or 14.7psi)
  • With a surface temperature of 15 ºC
  • At sea level
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8
Q

Four forces acting on an Aircraft/

A
  • Lift = or >Weight

- Thrust = or > Drag

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9
Q

What is Lift?

A

Lift is a mechanical force, Lift is generated by the difference in velocity between the solid body and the fluid

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10
Q

Newton’s second law of motion states that a force is produced when

A

A mass is accelerated.
F= m*a
Acceleration is a change in velocity over time.
F= m * ΔV / Δt

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11
Q

Factors That affect Lift ?

A

-The object= shape and size
-The motion=Velocity and inclination to flow
The air= mass, viscosity, compressibility

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12
Q

What is Drag ?

A

The resistance of the air to the motion of the aircraft,drag is directed along and opposed to the direction of flight.

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13
Q

Inter fence Drag is ?

A

Interference drag is incurred as one surface interferes with another in relationship to airflow

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14
Q

Parasite Drag is ?

A

The sum of all the drags not directly associated with the development of lift; such as friction, form and interference

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15
Q

Induce drag is?

A

Is commonly referred to as the drag produced by lift itself.

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16
Q

Total drag is ?

A

The sum then of all parasitic drag and all induced drag i

17
Q

Skin friction Drag

A

Reaction to the retardation of the flow within the boundary layer is skin friction drag.

18
Q

Winglet devise is used to control?

A

Winngtip vortices and use them to make the wing more efficient.

19
Q

Ground Effect?

A

Ground effect is caused by ground interference with airflow patterns around an aircraft when the aircraft is within one wingspan of the ground. At too high of an approach speed the aircraft may float down the runway and run out of runway length