Schillo, Conny (2008) FEMMAS contribution Buckling of composite panels Deliverable BEOS 5.0 Manual. DLR-Interner Bericht. DLR-IB 131-2008/14. 49 S.
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Abstract
This document serves as a manual for the computer program BEOS (Buckling loads of Eccentrically stiffened Orthotropic Shells), version 5.0. In contrast to previous versions it is possible in version 5.0 to define strip-wise different skin properties for one panel. In that way, the skin stiffening effect of the stringer feet can be considered by adding the foot stiffness to the stiffness of the corresponding skin element. This approach was closer investigated and described in reference
Item URL in elib: | https://elib.dlr.de/54010/ | ||||||||
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Document Type: | Monograph (DLR-Interner Bericht) | ||||||||
Title: | FEMMAS contribution Buckling of composite panels Deliverable BEOS 5.0 Manual | ||||||||
Authors: |
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Date: | February 2008 | ||||||||
Open Access: | No | ||||||||
Number of Pages: | 49 | ||||||||
Status: | Published | ||||||||
Keywords: | BEOS, Buckling loads, stiffened Orthotropic Shells | ||||||||
HGF - Research field: | Aeronautics, Space and Transport (old) | ||||||||
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: | 25 Apr 2008 | ||||||||
Last Modified: | 27 Apr 2009 14:55 |
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