Show simple item record

dc.creatorWeaver, Edgar R.en_US
dc.date.accessioned2017-07-17T19:19:16Zen_US
dc.date.available2017-07-17T19:19:16Zen_US
dc.date.created1926-03-15en_US
dc.identifier.urihttp://hdl.handle.net/11200/48903
dc.descriptionThe object of this static test was to determine the structural strength of this airplane.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Serviceen_US
dc.relation.ispartofseriesAir Service information circular (Aviation) ; v. 6, no. 559en_US
dc.relation.ispartofseriesMcCook Field report ; Serial no. 2578en_US
dc.subjectBiplanesen_US
dc.subjectConsolidated aircraften_US
dc.subjectAirplanes--Testingen_US
dc.subjectAirplanes, Militaryen_US
dc.subjectAirplanes--Wingsen_US
dc.subjectAirplanes--Landing gearen_US
dc.subjectAileronsen_US
dc.subjectElevators (Airplanes)en_US
dc.subjectAirplanes--Tail surfacesen_US
dc.subjectAirplanes--Fuselageen_US
dc.subjectAirplanes--Control systemsen_US
dc.subjectAirplanes--Parts--Testingen_US
dc.subjectAeronautics--Systems engineeringen_US
dc.subjectAirplanes--Design and constructionen_US
dc.titleStatic test of Consolidated Aircraft Company's PT-1 airplane (airplane section report)en_US
dc.typeTexten_US


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record