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dc.creatorUnited States. Army. Air Service. Engineering Division.en_US
dc.date.accessioned2018-07-19T15:25:01Z
dc.date.available2018-07-19T15:25:01Z
dc.date.created1921-07-20en_US
dc.identifier.urihttp://hdl.handle.net/11200/49163
dc.descriptionThe object of this test was to determine the strength of the wings, ailerons, empennage, fuselage, and landing chassis of the Curtiss night pursuit airplane, Type II.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Serviceen_US
dc.relation.ispartofseriesAir Service information circular (Aviation) ; v. 3, no. 266en_US
dc.relation.ispartofseriesMcCook Field report ; Serial no. 1603en_US
dc.subjectAirplanes, Militaryen_US
dc.subjectBiplanesen_US
dc.subjectCurtiss aircraften_US
dc.subjectAirplanes--Design and constructionen_US
dc.subjectAirplanes--Testingen_US
dc.subjectAirplanes--Parts--Testingen_US
dc.subjectStrength of materialsen_US
dc.subjectAirplanes--Control surfacesen_US
dc.subjectAirplanes--Fuselageen_US
dc.subjectAirplanes--Landing gearen_US
dc.subjectAirplanes--Wingsen_US
dc.subjectAileronsen_US
dc.subjectAeronautics--Systems engineeringen_US
dc.titleReport of static test of Curtiss night pursuit airplane, type II (airplane section, S. & A. branch)en_US
dc.typeTexten_US


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