Theory of Flight Flashcards
5 parts of aircraft structure
- fuselage (body)
- wings (lifting surface)
- tail (control surfaces)
4.propulsion (engine+prop) - landing gear (fixed vs. retractable)
angle of attack
relative airflow compared to chord line (line from leading to trailing edge)
depends on airflow, not attitude (airflow not always horizontal)
angle of incidence
chord line relative to horizontal datum line (wings relative to body)
centre of pressure
sum of aerodynamic pressure
higher angle of attack = higher pressure difference
past critical = decreased pressure
types of drag
- induced (wake turbulence from lift)
parasite (caused by anything but lift) - interference (2 surfaces meet at sharp angle e.g. struts)
- profile (shape causes e.g. skin friction)
aspect ratio
wing span / wing chord
(higher aspect = lower induced drag)
aileron
controls roll
aileron inside of turn lifts up
elevator
controls pitch (elevator down = nose down)
rudder
controls yaw
types of stability
stable, neutral, unstable
adverse yaw - torque
prop rotates clockwise so plane will yaw left
adverse yaw - asymmetric thrust
down prop will produce more lift so will yaw left
adverse yaw - precession
prop acts like gyroscope (yaw left)
adverse yaw - slipstream
air pushed by prop has corkscrew (tail right, nose left)
adverse yaw - aileron drag
when rolling one wing creates more lift (more drag)
causes yaw in opposite direction of turn
weight + balance too far aft
tail heavy, not enough forward elevator to recover stall
weight + balance too far forward
not enough back elevator control to recover descent
Va
maneuvering speed
Vs
stall speed (start of green)
Vy
best angle of climb (time)
Vx
best angle of climb (distance)
Vfe
max. flap extension speed
Vno
max. structural cruising speed