by Nexus » Mon Oct 04, 2004 7:10 am
Coffin corner occurs at an aircrafts absolute ceiling, where the speeds at which mach number buffet and prestall buffet occur, are the same
For a constant mach number, the IAS decreases with altitude due to decreaing LSS. To prevent the IAS from deacreasing to its stall speed, the mach number must be increased, which results in an increase in IAS.
But if you fly a constant IAS (in climb), the mach number will be increased to a point where it exceeds Mcrit, to prevent this from happen the IAS must be reduced.
So simply put, there comes a point at the aircrafts absolute ceiling where the aircraft can't go any higher. Because it is bounded
Last edited by
Nexus on Mon Oct 04, 2004 10:24 am, edited 1 time in total.