Written Test Question from FIA

innovator152

Well-Known Member
If the airspeed increases and decreases during longitudinal phugoid oscillations, the aircraft

B - is maintaining a nearly constant angle of attack.


just wondering if anyone here could help explain why that is the way it is, thanks.
 
What were the other two answer choices? Sometimes the FAA doesn't give the exact right answer as a choice but something close, or the "best choice". I think it may be one of those scenarios because the answer you posted says the aircraft "is maintaining a nearly constant angle of attack." The deal with Phugoid Oscillations is it's a really slow interchange of velocity and height about some equilibrium energy level as the aircraft attempts to re-establish the equilibrium level-flight condition from which it had been disturbed.

I think that there is in fact a change in AOA but because it is so slow the inertia forces and damping forces are very low and not perceived by the pilot.

:popcorn:
 
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