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Indicated airspeed is what matters, if indicated is high enough then cooling will be sufficient.
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Why don't you take the time to explain the relationship of Indicated airspeed, True airspeed, and altitude?
Then take some to explain the general behavior of a altitude effects on thrust production at constant power setting and indicated airspeed.
After you have done that, you can sum it all up as:
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Crumpp says:
The higher you go, the less effective the cooling due to pressure and density reduction despite the cooler temperatures.
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