Basics Flashcards

1
Q

Static air pressure and dynamic air pressure are…

A

Indirectly proportional

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2
Q

Increased dynamic air pressure is

A

Increased speed of air

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3
Q

Low air pressure is ____ the wing and high air pressure is _____ the wing

A

Above And below

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4
Q

what makes Angle ofattack?

A

angle between chord line and relative air flow

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5
Q

formula for lift

A

Angle of attack x half air density x Velocity(airspeed) squared x surface area of wing

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6
Q

if airspeed inreases then angle of attack must

A

decrease and vice versa

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7
Q

3 axes of movement

A

longitudinal, latitudinal, normal

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8
Q

what do you call rotation about the:
longitudinal
lateral
normal

A

Roll
pitch
yaw

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9
Q

Forces acting on a flying plane and directions they act in

A

Drag (backwards) , thrust (forward), lift (upwards), weight(downwards)

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10
Q

What axis does the stabilator control and what are the primary and secondary effects it causes

A

lateral axis
pitch
airspeed altitude

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11
Q

What axis does the aileron control and what are the primary and secondary effects it causes

A

longitudinal
roll
yaw

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12
Q

What axis does the rudder control and what are the primary and secondary effects it causes

A

normal
yaw
roll

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13
Q

types of drag

A

Induced drag
Parasite drag
- form
- skin friction
- interference

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14
Q

form drag is caused by

A

abstruction to smooth air flow eg dangling wheels

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15
Q

interference drag

A

when different airflows of different speeds clash

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16
Q

WHen is stall reached?

A

when angle of attack is exceeded
16 degrees

17
Q
A