Abstract
An analysis procedure of general cross-section properties is presented. The formulation
is based on the stress-strain states in the classic six equilibrium modes of a beam by
considering a finite thickness slice modelled by a single layer of 3D finite elements. The
theory is illustrated by application to composite sections of various shapes and material
layups.
Original language | English |
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Title of host publication | Proceedings of 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference |
Number of pages | 9 |
Publisher | American Institute of Aeronautics and Astronautics |
Publication date | 2015 |
DOIs | |
Publication status | Published - 2015 |
Event | 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference - Gaylord Palms and Convention Center, Kissimmee, United States Duration: 5 Jan 2015 → 9 Jan 2015 |
Conference
Conference | 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference |
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Location | Gaylord Palms and Convention Center |
Country/Territory | United States |
City | Kissimmee |
Period | 05/01/2015 → 09/01/2015 |