Or you change the shape of the wing and move the chord line by, say, lowering the flaps.
Draw a line between the leading and trailing edge and the angle changes compared to the attitude when you move the flaps.
Depends on how you define "angle of attack", eh?
Geoff
I'm another immigrant from RAP. Sounds like some good discussion here.
Lowering the flaps changes the angle of incidence of the inner wingspan, so its AOA increases relative to the rest of the wing. However, the camber is also greatly increased so the stall speed for the whole thing actually drops some, around 5 knots in a 172 at 40 degrees, most of which happens in the first 20 degrees. Most wings are designed to stall at the roots first, so stall behavior with flaps up or down isn't much different except that the deck angle will be lower with flaps extended.
Stalling on final is a rare problem. (Stalling and spinning while turning base is a different problem altogether, caused by skidding the airplane.) Most problems arise out of approaching too fast and getting into ground effect and either floating forever or it gets landed three-point and raises the risk of porpoising or wheelbarrowing or skidding the tires while trying to stop or just ending up in the rhubarb. And too much speed often comes from being too high and diving at the runway to get down. Doesn't work.
The POH has approach speeds listed, and those are plenty high enough. And THAT speed should be bled off close to the threshold before getting into ground effect. It's called the round-out and the textbooks describe it. The flare comes after the round-out. Two different things, but seamlessly put together.
A 172 would have a hard time getting to stall angle in the landing flare. We've had students drag the tail in the soft-field landing flare using a little power. The airplane is still flying. The $40 tail tiedown ring gets busted off. I get to fix those things that get busted by poor technique, and as an instructor as well as an engineer I get a little annoyed at times. Not a happy combination.
Angle of attack is difficult to determine while flying. The airplane's attitude is only part of it; the airplane's flight path is the rest, and you can have a high AOA with the nose level if you're slow enough to be sinking at a good rate. That's where airspeed control comes in.
Good landings start when you turn downwind. Plan ahead, get to the right altitude at the right places and the right speeds and everything improves enormously.
Dan
________
FJ1100