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Compressive strength of duralumin channels (airplane branch report)


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dc.creatorMiller, R. A.en_US
dc.date.accessioned2017-08-24T16:47:52Z
dc.date.available2017-08-24T16:47:52Z
dc.date.created1927-11-01en_US
dc.identifier.urihttp://hdl.handle.net/11200/48926
dc.descriptionThe purpose of this report is to record the results of tests of the compressive strength of duralumin channels, to recommend methods for their design, and to show the application of these methods to the design of channel-trussed beams. Conclusion: Shape effect, as a controlling factor in limiting the ultimate compressive strength of a duralumin channel, is not a question of thickness of material, radius of bend, or extent of flat sheet, but is a function of the ratios of the dimensions of the cross section to the gauge of the material.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Corpsen_US
dc.relation.ispartofseriesAir Corps information circular (Aviation) ; v. 6, no. 598en_US
dc.relation.ispartofseriesMateriel Division report ; Serial no. 2777en_US
dc.subjectDuralumin--Testingen_US
dc.subjectStrength of materialsen_US
dc.subjectStrains and stressesen_US
dc.subjectAirplanes--Parts--Testingen_US
dc.subjectAirplanes--Materials--Testingen_US
dc.subjectAirplanes--Design and constructionen_US
dc.subjectAeronautics--Systems engineeringen_US
dc.subjectAluminum tubes--Testingen_US
dc.titleCompressive strength of duralumin channels (airplane branch report)en_US
dc.typeTexten_US

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