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Spot welding and its application to aircraft structure corrosion-resistant steel 18:8 (materiel branch report)


Metadata FieldValueLanguage
dc.creatorHibert, Charles L.en_US
dc.date.accessioned2017-09-28T19:55:39Z
dc.date.available2017-09-28T19:55:39Z
dc.date.created1934-07-10en_US
dc.identifier.urihttp://hdl.handle.net/11200/49019
dc.descriptionThe corrosion resistance and tensile strength of spot welds in relation to their visual appearance and microscopic structure. A spot weld with adequate strength and ductility generally exhibits blow holes or gas holes in the fused zone, and splashes on the interior of the lap joint. Visual examination is inadequate for judging the quality or strength of spot welds.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Corpsen_US
dc.relation.ispartofseriesAir Corps information circular (Aviation) ; v. 7, no. 693en_US
dc.relation.ispartofseriesAir Corps technical report ; Serial no. 3907en_US
dc.subjectAirplanes--Weldingen_US
dc.subjectSteel--Weldingen_US
dc.subjectWelded joints--Testingen_US
dc.subjectMetal-worken_US
dc.titleSpot welding and its application to aircraft structure corrosion-resistant steel 18:8 (materiel branch report)en_US
dc.typeTexten_US

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