Tables of stiffness and carry-over factor for flat rectangular plates under compression

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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Bibliographic Details
Main Author: Kroll, W. D.
Corporate Authors: United States. National Advisory Committee for Aeronautics., Langley Aeronautical Laboratory.
Format: eBook
Language: English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1943]
Series: Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L398.
Subjects:
ISBN: 9781680156515
1680156519
Physical Description: 1 online resource (47 pages) : tables

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Summary: 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.
Item Description: 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.
Bibliography: Includes bibliographical references.
ISBN: 9781680156515
1680156519
Access: Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty