- 11 Μαρ 2019, 15:33
#570816
MACS software manages the rear horizontal stabilizer & apparently fails during high AOA turns... Software code for every contingency is not practical... yet.
https://en.wikipedia.org/wiki/Angle_of_attackAbove this critical angle of attack, the aircraft is said to be in a stall. A fixed-wing aircraft by definition is stalled at or above the critical angle of attack rather than at or below a particular airspeed. The airspeed at which the aircraft stalls varies with the weight of the aircraft, the load factor, the center of gravity of the aircraft and other factors. However the aircraft always stalls at the same critical angle of attack. The critical or stalling angle of attack is typically around 15° - 20° for many airfoils.
Some aircraft are equipped with a built-in flight computer that automatically prevents the aircraft from increasing the angle of attack any further when a maximum angle of attack is reached, regardless of pilot input. This is called the 'angle of attack limiter' or 'alpha limiter'. Modern airliners that have fly-by-wire technology avoid the critical angle of attack by means of software in the computer systems that govern the flight control surfaces.
Α ωραία , αντί για μπόμπες αρκεί ένα καλό χακάρισμα .
Οι κινέζοι καθήλωσαν τα δικά τους , οι αμερικάνοι και καναδοί όχι.
Τελευταία επεξεργασία από mousatos και 11 Μαρ 2019, 15:38, έχει επεξεργασθεί 1 φορά/ες συνολικά
Άμπερ αλέρτ . Αγνοείται εισαγγελέας.
