i thought ...
IAS was a measure of force of the air and relates to stress loads, lift, and in this case turn performance at relative altitudes.
i.e. speed limits related to forces ...
and ...
TAS is a measure of speed of the air and relates to airflow over the surfaces and how the surfaces and the air relates at different speeds.
i.e. speed limits relating to the ability for the air to flow "cleanly" over the surface of the aircraft.
that being the case i am unclear how TAS would be a determining factor of turn rate at altitude unless you guys are saying compression is coming into play ...
Stoney, I think I figured out how this works way back in our discussion about IAS vs TAS in P47 glide numbers.
Physics wise, the IAS speed will dictate how much lift the wing can generate. TAS is irrelevant for lift considerations if you have IAS available.
What TAS DOES affect though is your turn radius. You will pull a MUCH wider turn radius at high altitude for the same amount of Gs (i.e., lift).