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Transonic Flight

High Speed Aerodynamics

Indicated Airspeed (IAS)280 kt
Flight Level350
OAT-50 °C
Mach Number
0.872
True Airspeed: 508 KT
Local Speed of Sound
582 kt
Coffin Margin
187 kt
OVERSPEED (MACH BUFFET)

Flight Envelope

Coffin Corner Analysis
Low Speed Stall
Limit Mach (MMO)
STALL (Vs)
MMO (0.82)
FL600FL400FL200SL
0 KT198402600 KT (TAS)

The intersection of the Stall Speed (which increases with altitude) and the Critical Mach (which decreases in TAS with altitude) defines the absolute ceiling. In the "Coffin Corner", any increase in speed causes Mach Buffet, and any decrease causes Stall.