What are three components of a stall for aircraft?
Have a review sheet that I have to complete and this one question I am stuck on. My guess would be loss of lift, Criticle Angle of Attack, and Reducing pitch.
Have a review sheet that I have to complete and this one question I am stuck on. My guess would be loss of lift, Criticle Angle of Attack, and Reducing pitch.
?
Speed, weight, attitude.
Anonymous
Understand aerodynamics, you'll understand what to expect.
Anonymous
I cant think of 3 "components" but, several Causes:
1) excess angle of attack
2) airspeed below stall speed.
3) excess weight
4)load factor--weight & balance. This can cause excess pitch/AOA.
5) Center of gravity location--again, affected by loading, affects AOA
5) low engine power ( a Cause of low IAS)
Stall is caused by lack of sufficient lift; in cases of excess pitch/AOA, the laminar airflow over top of wing breaks into turbulence, so insufficient vacuum atop wing. Way to recover is almost always to pitch nose Downward (Counter-intuitive) and increase engine power. With the V- Tail Beech "Bonanza", it was handled Differently. . That's why so many crashes with them.
Old Man Dirt
"Stall" is the loss of lift and it has to do with speed and just how far up your nose is pointed. Not being schooled as a pilot, I can't think of the third.
Just please let us know when and where you are flying- because I don't want to be any where near the crash zone.
Starrysky
Reducing pitch is a cure, not a component of a stall. Better would be low air speed.