Abstract

THE staff of the Langley Memorial Aeronautical Laboratory, working under the direction of the National Advisory Committee for Aeronautics of America, have recently been undertaking continuous research into all aspects of the compression ignition engine. A series of reports has been issued lately covering certain sections of this research programme, and the results which have been obtained are of interest. They deal exclusively with the design of fuel injection nozzles, and there is no doubt that a systematic study of this sort provides information of assistance to engine designers.

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