10 Core Concepts of Flight
Lift = Weight, in unaccelerated flight
Angle of attack controls airspeed
Excess thrust controls
angle
of climb or descent
Excess power controls
rate
of climb or descent
The main purpose of flaps is to lower the aircraft's stall speed
Load factor = Lift/Weight
Steady wind has no aerodynamic effect on an airplane
Centrifugal force is a fictitious force
The wing sees
calibrated
airspeeds
Ground effect is a reduction in drag, not an increase in lift