elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Contact | Deutsch
Fontsize: [-] Text [+]

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.

Full text not available from this repository.


Item URL in elib:https://elib.dlr.de/16249/
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 AuthorsAuthors ORCID iD
Geier, B.UNSPECIFIEDUNSPECIFIED
Singh, G.UNSPECIFIEDUNSPECIFIED
Date:1997
Journal or Publication Title:Aerospace Science and Technology
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
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: DLR-Beauftragter, elib
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 15:32

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
electronic library is running on EPrints 3.3.12
Copyright © 2008-2017 German Aerospace Center (DLR). All rights reserved.