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Validation procedure for nonlinear analysis of stringer stiffened CFRP Panels

Kling, Alexander and Teßmer, Jan and Degenhardt, Richard (2006) Validation procedure for nonlinear analysis of stringer stiffened CFRP Panels. 25th Congress of International Council of the Aeronautical Science, 2006-09-03 - 2006-09-08, Hamburg, Deutschland.

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Item URL in elib:https://elib.dlr.de/47207/
Document Type:Conference or Workshop Item (Paper)
Title:Validation procedure for nonlinear analysis of stringer stiffened CFRP Panels
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Kling, AlexanderUNSPECIFIEDUNSPECIFIED
Teßmer, JanUNSPECIFIEDUNSPECIFIED
Degenhardt, RichardUNSPECIFIEDUNSPECIFIED
Date:September 2006
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Keywords:CFRP, panel, buckling load, postbuckling
Event Title:25th Congress of International Council of the Aeronautical Science
Event Location:Hamburg, Deutschland
Event Type:international Conference
Event Dates:2006-09-03 - 2006-09-08
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research (old)
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Structures & Materials (old)
Location: Braunschweig
Institutes and Institutions:Institute of Composite Structures and Adaptive Systems > Structural Mechanics
Deposited By: Ries, Doris
Deposited On:07 Nov 2007
Last Modified:31 Jul 2019 19:18

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