The stability under longitudinal compression of flat symmetric corrugated-core sandwich plates with simply supported loaded edges and simply supported or clamped unloaded edges

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Bibliographic Details
Main Author Seide, Paul (Author)
Corporate Authors Langley Aeronautical Laboratory, United States. National Advisory Committee for Aeronautics
Format Electronic eBook
LanguageEnglish
Published Washington, D.C. : National Advisory Committee for Aeronautics, 1952.
SeriesTechnical note (United States. National Advisory Committee for Aeronautics) ; no. 2679.
Subjects
Online AccessFull text
ISBN9781680156249
1680156241
Physical Description1 online resource (30 pages) : illustrations

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