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dc.creatorWeaver, Edgar R.en_US
dc.date.accessioned2016-05-10T20:39:25Z
dc.date.available2016-05-10T20:39:25Z
dc.date.created1925-06-15en_US
dc.date.issued1925-06-15en_US
dc.identifier.urihttp://hdl.handle.net/11200/48594
dc.descriptionThis test was conducted for the purpose of determining the strength of this experimental spar relative to its weight. ... This Engineering Division steel tube spar is structurally satisfactory with the exception of the inner end fitting.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Serviceen_US
dc.relation.ispartofseriesAir Service information circular (Aviation) ; v. 6, no. 519en_US
dc.relation.ispartofseriesMcCook Field report ; Serial no. 2471en_US
dc.subjectAeronautics--Researchen_US
dc.subjectAeronautics--Systems engineeringen_US
dc.subjectAirplanes--Design and constructionen_US
dc.subjectAirplanes--Materials--Testingen_US
dc.subjectStrength of materials
dc.subjectAirplanes--Parts--Testing
dc.subjectAirplanes--Wings
dc.titleStatic test of the Engineering Division experimental steel spar designed by I.M. Landon (airplane section report)en_US
dc.typeTexten_US


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