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Some Simple Solutions for Buckling Loads of Thin and Moderately Thick Cylindrical Shells and Panels Made of Laminated Composite Material

Geier, B. and Singh, G. (1997) Some Simple Solutions for Buckling Loads of Thin and Moderately Thick Cylindrical Shells and Panels Made of Laminated Composite Material. Aerospace Science and Technology, Vol. 1 (1), pp. 47-63.

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Document Type:Article
Additional Information: LIDO-Berichtsjahr=1999,
Title:Some Simple Solutions for Buckling Loads of Thin and Moderately Thick Cylindrical Shells and Panels Made of Laminated Composite Material
Authors:
AuthorsInstitution or Email of Authors
Geier, B.UNSPECIFIED
Singh, G.UNSPECIFIED
Date:1997
Journal or Publication Title:Aerospace Science and Technology
Refereed publication:Yes
In ISI Web of Science:Yes
Volume:Vol. 1
Page Range:pp. 47-63
Status:Published
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:other
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:no assignment
DLR - Research theme (Project):UNSPECIFIED
Location: Braunschweig
Institutes and Institutions:Institute of Composite Structures and Adaptive Systems > Institut für Strukturmechanik
Deposited By: elib DLR-Beauftragter
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 15:32

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