terça-feira, 3 de novembro de 2026

COFFIN CORNER = STALL SPEED INCREASES WITH ALTITUDE + CRITICAL MACH NUMBER DECREASES WITH ALTITUDE

 


Click on the image to see it isolated and amplified

When a jet aircraft captain decides to fly at an altitude very close to the operational ceiling of the aircraft, the risks are increased due to the environment of this flight being within the area called the "coffin corner", which is formed by the apexes of the stall speed curves and the Mach number curve.

Look in the image showing the two Cartesians’ curves almost joining at the top of the curves.

All it takes is gusty turbulence, a steep curve, ice formation, or an incorrect speed adjustment can push the plane against one of the curves, what means very high possibility to lose the jet plane flight controls. 

You must descend gradually [around 1500 feet per minute] to flight level around 25,000 feet to keep the plane at the safety zone of the envelope formed by the two: stall speed and Mach number Cartesian’s curves.

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