Nonlinear finite element analysis of thermal post-buckling vibration of laminated composite shell panel embedded with SMA fibre

Gespeichert in:

Autor*in:	Panda, Subrata Kumar [verfasserIn] Singh, B.N.

Format:	Artikel

Erschienen:	2013

Umfang:	11

Übergeordnetes Werk:	Enthalten in: Aerospace science and technology - Paris : Elsevier, 1997, 29(2013), 1 vom: Aug., Seite 47-57
Übergeordnetes Werk:	volume:29 ; year:2013 ; number:1 ; month:08 ; pages:47-57 ; extent:11

Katalog-ID:	OLC1925331393

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