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NASA-TR-R-30

LOCAL INSTABILITY OF THE ELEMENTS OF A TRUSS-CORE SANDWICH PLATE

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1959

Abstract: The charts presented give the compressive buckling coefficients for a single-truss-core and a double-truss-core sandwich plate. These charts cover a wide range of sandwich proportions and may be used for sandwiches with unequal faces. They apply to in-plane compressive loads acting parallel or perpendicular to the core direction or for various combinations of these loads.
URI: https://yse.yabesh.ir/std/handle/yse/63444
Subject: BUCKLING
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  • NASA - National Aeronautics and Space Administration (NASA)
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    NASA-TR-R-30

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:00:18Z
date available2017-09-04T16:00:18Z
date copyright01/01/1959
date issued1959
identifier otherRHYHUEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/63444
description abstractThe charts presented give the compressive buckling coefficients for a single-truss-core and a double-truss-core sandwich plate. These charts cover a wide range of sandwich proportions and may be used for sandwiches with unequal faces. They apply to in-plane compressive loads acting parallel or perpendicular to the core direction or for various combinations of these loads.
languageEnglish
titleNASA-TR-R-30num
titleLOCAL INSTABILITY OF THE ELEMENTS OF A TRUSS-CORE SANDWICH PLATEen
typestandard
page18
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1959
contenttypefulltext
subject keywordsBUCKLING
subject keywordsCHARTS
subject keywordsCOEFFICIENTS
subject keywordsCOMPRESSIBILITY
subject keywordsLOADS (FORCES)
subject keywordsSANDWICH STRUCTURES
subject keywordsTRUSSES
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