Buckling Load Reduction for Stiffened Panels Due to Cutouts in Ribs

Gespeichert in:

Autor*in:	Watson, A. [verfasserIn] Williams, F.W. Kennedy, D.

Format:	Artikel

Erschienen:	1998

Umfang:	3

Übergeordnetes Werk:	Enthalten in: AIAA journal / American Institute of Aeronautics and Astronautics - Reston, Va. [u.a.] : AIAA, 1963, 36(1998), 2, Seite 264-266
Übergeordnetes Werk:	volume:36 ; year:1998 ; number:2 ; pages:264-266 ; extent:3

Katalog-ID:	OLC1529815630

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Buckling Load Reduction for Stiffened Panels Due to Cutouts in Ribs

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