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Buckling of a Flanged Plate

descriptionPublicationkeyboard_double_arrow_right Article 01 Apr 1946 English Publisher:American Institute of Aeronautics and Astronautics (AIAA)Journal:Journal of the Aeronautical Sciences, volume 13, pages 187-191 (eissn: 1936-9956, Copyright policy )
Authors: HENRY L. LANGHAAR;

doi: 10.2514/8.11344

Buckling of a Flanged Plate

Abstract

This investigation treats the buckling of an axially compressed isotropic elastic rectangular plate tha t is hinged on the ends, supported bu t subjected to elastic rotational restraint on one longitudinal edge, and flanged but otherwise free on the remaining edge. A numerical procedure with a rigorous mathematical basis is proposed for solving elastic stability problems of this type.

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selected citations
These citations are derived from selected sources.
This is an alternative to the "Influence" indicator, which also reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
BIP!Citations provided by BIP!
popularity
This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network.
BIP!Popularity provided by BIP!
influence
This indicator reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
BIP!Influence provided by BIP!
impulse
This indicator reflects the initial momentum of an article directly after its publication, based on the underlying citation network.
BIP!Impulse provided by BIP!
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