Theory of Flight Flashcards

1
Q

5 parts of aircraft structure

A
  1. fuselage (body)
  2. wings (lifting surface)
  3. tail (control surfaces)
    4.propulsion (engine+prop)
  4. landing gear (fixed vs. retractable)
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2
Q

angle of attack

A

relative airflow compared to chord line (line from leading to trailing edge)
depends on airflow, not attitude (airflow not always horizontal)

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3
Q

angle of incidence

A

chord line relative to horizontal datum line (wings relative to body)

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4
Q

centre of pressure

A

sum of aerodynamic pressure

higher angle of attack = higher pressure difference
past critical = decreased pressure

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5
Q

types of drag

A
  1. induced (wake turbulence from lift)
    parasite (caused by anything but lift)
  2. interference (2 surfaces meet at sharp angle e.g. struts)
  3. profile (shape causes e.g. skin friction)
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6
Q

aspect ratio

A

wing span / wing chord
(higher aspect = lower induced drag)

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7
Q

aileron

A

controls roll
aileron inside of turn lifts up

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8
Q

elevator

A

controls pitch (elevator down = nose down)

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9
Q

rudder

A

controls yaw

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10
Q

types of stability

A

stable, neutral, unstable

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11
Q

adverse yaw - torque

A

prop rotates clockwise so plane will yaw left

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12
Q

adverse yaw - asymmetric thrust

A

down prop will produce more lift so will yaw left

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13
Q

adverse yaw - precession

A

prop acts like gyroscope (yaw left)

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14
Q

adverse yaw - slipstream

A

air pushed by prop has corkscrew (tail right, nose left)

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15
Q

adverse yaw - aileron drag

A

when rolling one wing creates more lift (more drag)
causes yaw in opposite direction of turn

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16
Q

weight + balance too far aft

A

tail heavy, not enough forward elevator to recover stall

17
Q

weight + balance too far forward

A

not enough back elevator control to recover descent

18
Q

Va

A

maneuvering speed

19
Q

Vs

A

stall speed (start of green)

20
Q

Vy

A

best angle of climb (time)

21
Q

Vx

A

best angle of climb (distance)

22
Q

Vfe

A

max. flap extension speed

23
Q

Vno

A

max. structural cruising speed