akafrank07
11th Oct 2012, 20:06
"Mach number is used as a speed reference at high altitudes, usually above 26000 ft, because the MN becomes the aircraft's limiting speed in preference to IAS. That is, up to approximately 26000 ft, an aircraft will climb at a constant IAS against an increasing MN, where the MN speed reaches the aircraft's MN limiting speed. Then above 26000 ft the aircraft is flown at a constant MN with a decreasing IAS for an increase in altitude."
From the above i take it that the mach number limiting speed is the mach number speed that you reach when you change from IAS to MN?
I would i also to right in saying when you are climbing at a constant IAS to 26000 ft your TAS would always have to be increasing due to ram air affects and also the density becoming less meaning you would have to fly faster to keep the indicated airspeed constant?
Cheers
From the above i take it that the mach number limiting speed is the mach number speed that you reach when you change from IAS to MN?
I would i also to right in saying when you are climbing at a constant IAS to 26000 ft your TAS would always have to be increasing due to ram air affects and also the density becoming less meaning you would have to fly faster to keep the indicated airspeed constant?
Cheers