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dc.contributor.advisorWise, Joseph A.
dc.contributor.authorRobinson, Gerald A.
dc.dateAugust 31, 1949
dc.date.accessioned2012-03-14T17:52:02Z
dc.date.available2012-03-14T17:52:02Z
dc.date.issued1949-08-31
dc.identifier.urihttp://hdl.handle.net/10945/6334
dc.descriptionThis thesis document was issued under the authority of another institution, not NPS. At the time it was written, a copy was added to the NPS Library collection for reasons not now known. It has been included in the digital archive for its historical value to NPS. Not believed to be a CIVINS (Civilian Institutions) title.en_US
dc.description.abstractThe design of an arrangement for applying uniformly distributed biaxial loads to a plate where the plate edges are simply supported is presented; the behavior of a sandwich plate (Metalite) when it is subjected to this type of load and edge conditions is presented. The method of transformed sections is utilized to predict the plate critical load for the sandwich plate (Metalite); a comparison is made between the value predicted by this method and that predicted from laboratory testing with the leading arrangement. Principal strains and principle stresses at selected points on the surface of the plate are presented; deflections of these selected points also are included.en_US
dc.description.urihttp://www.archive.org/details/behaviorofmetali00robi
dc.language.isoen_US
dc.publisherSt. Paul, Minnesota; University of Minnesotaen_US
dc.subject.lcshAeronauticsen_US
dc.titleThe behavior of a metalite plate when subjected to unformly distributed loads acting in the plane of the plate.en_US
dc.typeThesisen_US
dc.contributor.corporateUniversity of Minnesota
dc.contributor.departmentDepartment of Aeronautical Engineering
dc.description.serviceLieutenant Commander, United States Navy .en_US
etd.thesisdegree.nameM.S. in Aeronautical Engineeringen_US
etd.thesisdegree.levelMastersen_US
etd.thesisdegree.disciplineAeronautical Engineeringen_US
etd.thesisdegree.grantorUniversity of Minnesotaen_US
etd.verifiedyesen_US


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