Originally posted by GScholz
*LOL* What you need to understand is that you are not in space at 25K feet. You have 50% of the air molecules, but those molecules are considerably cooler than at SL and carry away a greater amount of heat than the 100% amount of hotter molecules at SL.
The P-38 did not have any problems with keeping the engines warm at low and medium altitudes, but at high altitudes it did. QED.
You describe a cooling system that was poorly designed and had a problem with allowing the oil to warm up, yet you insist on using that to somehow convince me as to the laws of thermal dynamics and to the lower cooling ability of lower air density (by the way it is less then half the air density at 30k feet more like 80% less).
I have first hand knowledge of this and have flown as pilot in command many times in the low 20's and have seen both higher EGT and CHT levels higher with altitude as well as TIT rise on the turbo. I have opened the cowl flaps a bit and added mixture as well as lowering MP to help keep them in limits.
I will say it has been fun playing, have a good day and regards friend:)