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FEMMAS contribution Buckling of composite panels Deliverable BEOS 5.0 Manual

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

Document Type:Monograph (DLR-Interner Bericht)
Title:FEMMAS contribution Buckling of composite panels Deliverable BEOS 5.0 Manual
Authors:
AuthorsInstitution or Email of Authors
Schillo, ConnyUNSPECIFIED
Date:February 2008
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
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Structures & Materials
Location: Braunschweig
Institutes and Institutions:Institute of Composite Structures and Adaptive Systems > Structural Mechanics
Deposited By: Doris Ries
Deposited On:25 Apr 2008
Last Modified:27 Apr 2009 14:55

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