I would like to know how engines cooling is calculated in AH2.
I do understand that a liquid cooled engine under normal circumstances cool off faster.
How does altitude impact on cooling temps ?
I mean, air-cooled engines normally shock-cool if you leave them at idle at higher altitudes IRL, if my memory serves me right.
I will take an example.
Fw190a8 will, if red-lined, be pretty much be useless for the next 5-10 minutes ( Wep is life in that bird), you might as well go and change plane whereas other air-cooled planes cool off relatively fast.