PoF Chapter 7 Stall

airflow separation

low airspeed

high angle of attack

low density

16 degrees

12 degrees

10 degrees

30 degrees

angle of attack must be reduced

angle of attack must be increased

bank angle must be increased

density must be increased

stalls at the wing tip first and causes the aircraft to pitch up

stalls at the wing tip first and causes the aircraft to pitch down

stalls at the wing root first and causes the aircraft to pitch up

stalls at the wing root and causes the aircraft to pitch down

increase

decrease

stay constant

decrease then increase

at a slower stall speed

at a higher stall speed

at the same stall speed

at any speed

the CP moves aft and the aircraft pitches down

the CP moves aft and the aircraft pitches up

the CP moves forward and the aircraft pitches up

the CP moves forward and the aircraft pitches down

at the wing tip first

at the wing root first

at the leading edge first

at the trailing edge first

induce stall at the wing root

induce stall at the wing tip

delay stall at the wing root

delay stall at the leading edge

15 degrees

20 degrees

25 degrees

30 degrees