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هوافضا::
آدیاباتیک
corrected for the adiabatic temperature riso resulting from the airplano speed: -
Adiabatic Compression
The temperature at the radiator-tube entrance is given by a statement of the law of the conservation of energy for the adiabatic flow of a.perfect gas
Because the heat generated by viscous shearing forces is quadratically dependent on the cooling-air velocity, this heat becomes appreciable at high airspeeds. 5,011 sucil cases Crocco gives the following rule in reference 4: "The transference of heat between any object and a fluid ft owing by it, when it is no longer possible to disre- card the heat developed by friction, is governed by the same law that applied when it is negligible, provided the temperature to which the fluid is brought by adiabatic arrest is considered as its temperature."
adiabatic efficiency of supercharger •
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