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Tables of stiffness and carry-over factor are presented for infinitely long flat plates subjected to a uniformly distributed longitudinal compressive load. The tables are intended for use in solving problems in the stability of structures composed of plates under compression.
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Tables of stiffness and carry-over factor for flat rectangular plates under compression
1943, National Advisory Committee for Aeronautics
in English
1680156519 9781680156515
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Edition Notes
NACA Wartime Report L-398.
Originally issued as NACA as Advance Restricted Report L3K27 (November 1943).
Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia.
Includes bibliographical references.
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