I want to know why. It just does not make sense.
Because the air is thinner
It’s quite the complex thing, but ol’ @Brandon_Sandstrom composed this tutorial back in the days per my request to explain it all better:
thanks a lot
GS has no bearing on the aircraft only dynamic pressure as you will come to understand by reading the tutorial @schyllberg posted.
This statement is wrong.
Someone needs to read the tutorial it seems ;)
Also incorrect the only reason you see a decrease in the IAS limitation above FL280 is because you are transitioning to Mach speed and reaching that limitation before the other.
Just realized the issues with that statement, ouch.
Because the airspeed limit is higher than the mach limit so the mach limit takes over.
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