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dc.creatorUnited States. Army. Air Service. Engineering Division.en_US
dc.date.accessioned2018-08-08T20:14:53Z
dc.date.available2018-08-08T20:14:53Z
dc.date.created1922-03-15en_US
dc.identifier.urihttp://hdl.handle.net/11200/49227
dc.descriptionThe purpose of this test was to develop a carburetor setting for the Liberty 12- cylinder engine adapting it for dirigible service. The recommended carburetor setting to be used in conjunction with the Zenith U.S. 52 carburetors i 24-millimeter chokes, 1.15 millimeter main jets, and 1.20 millimeter compensator jets. This setting is to be used to obtain approximately 280 horsepower at 1,400 revolutions per minute. At this output the Liberty engine will weigh 3 pounds per horsepower.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Serviceen_US
dc.relation.ispartofseriesAir Service information circular (Aviation) ; v. 4, no. 311en_US
dc.relation.ispartofseriesMcCook Field report ; Serial no. 1732en_US
dc.subjectCarburetors--Testingen_US
dc.subjectAirshipsen_US
dc.subjectBalloonsen_US
dc.subjectAirplanes--Motors--Testingen_US
dc.subjectAirplanes--Parts--Testingen_US
dc.subjectAirplanes--Motors--Partsen_US
dc.subjectAirplanes--Motors--Carburetorsen_US
dc.titleThe determination of a carburetor setting for the Liberty engine for dirigible use (power plant section report)en_US
dc.typeTexten_US


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