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dc.creatorUnited States. Army. Air Service. Engineering Division.en_US
dc.date.accessioned2017-12-07T16:59:12Z
dc.date.available2017-12-07T16:59:12Z
dc.date.created1920-11-20en_US
dc.identifier.urihttp://hdl.handle.net/11200/49100
dc.descriptionThe object of this test was to determine whether or not the Packard fuelizer as applied to the Liberty engine is effective for use in flight, principally with regard to giving good acceleration when the engine is opened up after a glide. It is concluded that in its present form the Packard fuelizer applied to the Liberty engines is unsatisfactory for service use.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Serviceen_US
dc.relation.ispartofseriesAir Service information circular (Aviation) ; v. 2, no. 134en_US
dc.relation.ispartofseriesMcCook Field report ; Serial no. 1355en_US
dc.subjectAirplanes--Parts--Testingen_US
dc.subjectAirplanes--Motors--Partsen_US
dc.subjectAirplanes--Fuel systemsen_US
dc.titleFlight test of Packard fuelizer on Liberty "12"en_US
dc.typeTexten_US


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