Tables of stiffness and carry-over factor for flat rectangular plates under compression
By: W.D. Kroll
Contributors: United States. National Advisory Committee for Aeronautics; Langley Aeronautical Laboratory
Series: Wartime Report / National Advisory Committee for Aeronautics -- no. L398; Wartime Reports (United States. National Advisory Committee for Aeronautics) -- no. L398.
Publisher: National Advisory Committee for Aeronautics
Published: 1943
Place of publication: Washington, D.C
Language: eng
Number of pages: 47
ISBN-13: 9781680156515
Subjects: Plates (Engineering); Axial loads; Loads (Mechanics); Buckling (Mechanics); Stability; Plaques (Ingénierie); Charges axiales; Charges; Flambage (Résistance des matériaux); Stabilité; Warping; Buckling
Other titles: NACA Wartime Reports. Series L.
Description: 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.
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.