Ten-hour endurance test of Lawrance all-aluminum cylinder (power plant section report)

Metadata Field	Value	Language
dc.creator	United States. Army. Air Service. Engineering Division.	en_US
dc.date.accessioned	2018-08-06T15:13:48Z
dc.date.available	2018-08-06T15:13:48Z
dc.date.created	1921-03-25	en_US
dc.identifier.uri	http://hdl.handle.net/11200/49213
dc.description	The object of this test was to determine the reliability and durability of an all-aluminum alloy cylinder on the Lawrance 3-cylinder engine. The cylinder performed satisfactorily, on the torque stand, for a period of 10 hours, except for the exhaust-valve seat, which was hammered out badly. There appears to be no advantage gained in cooling, due to the all-aluminum construction.	en_US
dc.format	PDF	en_US
dc.publisher	Washington, D.C. : Chief of Air Service	en_US
dc.relation.ispartofseries	Air Service information circular (Aviation) ; v. 2, no. 192	en_US
dc.relation.ispartofseries	McCook Field report ; Serial no. 1427	en_US
dc.subject	Airplanes--Motors--Cylinders	en_US
dc.subject	Airplanes--Parts--Testing	en_US
dc.subject	Airplanes--Design and construction	en_US
dc.subject	Aeronautics--Systems engineering	en_US
dc.subject	Aluminum alloys	en_US
dc.subject	Airplanes--Motors--Parts	en_US
dc.title	Ten-hour endurance test of Lawrance all-aluminum cylinder (power plant section report)	en_US
dc.type	Text	en_US

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