THE need of intake-charge cooling for the suppression of detonation in highly supercharged engines is indicated by the authors of this paper. The relation of detonation-limited output to intake-charge temperature under numerous engine design and operating conditions is illustrated.Several different methods of reducing the intake-charge temperature are discussed and evaluated, special emphasis being put on the use of intercoolers, aftercoolers, and secondary-liquid injection. It is shown that the choice of any one of these methods depends largely on the type of engine installation and the use of the airplane.
The RELATION COOLING of INTAKE-CHARGE to ENGINE PERFORMANCE
Sae Technical Papers
Pre-1964 SAE Technical Papers ; 1906
01.01.1944
Aufsatz (Konferenz)
Englisch
Relation of intake charge cooling to engine performance
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