This Is AuburnAUrora

Show simple item record

Static test of the Curtiss XO-1 observation airplane (airplane section report)


Metadata FieldValueLanguage
dc.creatorWeaver, D. B.en_US
dc.date.accessioned2017-06-22T18:04:25Z
dc.date.available2017-06-22T18:04:25Z
dc.date.created1925-10-01en_US
dc.identifier.urihttp://hdl.handle.net/11200/48831
dc.descriptionThis static test was conducted for the purpose of determining the structural strength of the Curtiss XO-1 airplane submitted during the contest for corp-observation airplanes, December 1924, and purchased on contract No. 727. Tests included: wing cellule tests; leading edge static tests; ailerons tests; stabilizer and elevator tests; rudder and fin tests; landing chassis tests; fuel tank release mechanism tests; fuselage tests; tail skid impact tests. Results of the tests are reported, along with design recommendations based on those results.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Serviceen_US
dc.relation.ispartofseriesAir Service information circular (Aviation) ; v. 6, no. 539en_US
dc.relation.ispartofseriesMcCook Field report ; Serial no. 2523en_US
dc.subjectCurtiss aircraften_US
dc.subjectAirplanes--Testingen_US
dc.subjectAirplanes, Militaryen_US
dc.subjectElevators (Airplanes)en_US
dc.subjectAileronsen_US
dc.subjectAirplanes--Fuel systemsen_US
dc.subjectAirplanes--Fuselageen_US
dc.subjectAirplanes--Wingsen_US
dc.subjectAirplanes--Landing gearen_US
dc.subjectAirplanes--Partsen_US
dc.subjectAirplanes--Control surfacesen_US
dc.subjectAirplanes--Design and constructionen_US
dc.titleStatic test of the Curtiss XO-1 observation airplane (airplane section report)en_US
dc.typeTexten_US

Files in this item

This item appears in the following Collection(s)

Show simple item record