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dc.contributor.authorMechling, Wallace Bristol
dc.contributor.authorJack, Samuel Sloan
dc.date.accessioned2012-03-14T17:52:23Z
dc.date.available2012-03-14T17:52:23Z
dc.date.issued1938
dc.identifier.urihttp://hdl.handle.net/10945/6399
dc.descriptionNPS CIVINS (Civilian Institutions) Thesis documenten_US
dc.descriptionApproved for public release; distribution is unlimiteden_US
dc.description.abstractIn an endeavor to evaluate the Tension Impact Test and to correlate results, it was necessary to conduct the test upon material whose exact physical properties were known. It was decided to employ the purpose as a complete investigation of their properties had not been made available to the industry. Thus the routine tests conducted for correlation purposes have an added value in that they present further data on these alloys.en_US
dc.description.urihttp://www.archive.org/details/evaluationoftens00mech
dc.language.isoen_US
dc.publisherCalifornia Institute of Technologyen_US
dc.subject.lcshAeronauticsen_US
dc.titleAn evaluation of the tension impact test by correlation with the physical properties of aluminum alloysen_US
dc.typeThesisen_US
dc.contributor.departmentAeronautical Engineering
dc.description.funderNPS CIVINSen_US
dc.description.serviceLieutenant, United States Navyen_US
dc.description.serviceCaptain, United States Marine Corpsen_US
etd.thesisdegree.nameM.S. in Aeronautical Engineeringen_US
etd.thesisdegree.levelMastersen_US
etd.thesisdegree.disciplineAeronautical Engineeringen_US
etd.thesisdegree.grantorCalifornia Institute of Technologyen_US
etd.verifiedyesen_US


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