The stability under longitudinal compression of flat symmetric corrugated-core sandwich plates with simply supported loaded edges and simply supported or clamped unloaded edges / Paul Seide.
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Format: | Government Document eBook |
Language: | English |
Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1952.
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Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2679. |
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Call Number: |
TA660.P6
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TA660.P6 | Available |