A new strength model for application of a physically based failure criterion to orthogonal 3D fiber reinforced plastics
Source abstract
Abstract
A strength model for 3D fiber-reinforced plastics consisting of unidirectional layers with a high in-plane fiber density and additional reinforcements perpendicular to the layers with a significantly lower fiber density is presented. The strength model aims to enhance the application range of an existing, physically based failure criterion for inter-fiber fracture of unidirectional fiber-reinforced layers to the above mentioned configuration of 3D-composites. In doing so the fundamental physical basis, the fracture hypothesis of Mohr, and the general mathematical formulation of the criterion are sustained. The enhancement of the application range is achieved by employing a continuous interpolation between the basic strengths of an orthogonal 3D fiber-reinforced layer.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Mechanical Behavior of Composites · Composite Material Mechanics · Topology Optimization in Engineering
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References (8)
Show source-provided references
1. Failure criteria for unidirectional fiber composites10.1115/1.3153664 ↗
2. Puck · 1996
3. Mohr O. Welche Umstände bedingen die Elastizitätsgrenze und den Bruch eines Materials? Z. d. VDI, 1900; Vol. 24 (45) 1524–30 and (46) 1572–77.
4. Bruchbedingungen vom Mohrschen Typ für transversal-isotrope Werkstoffe am Beispiel der Faser-Kunststoff-Verbunde10.1002/zamm.19960760904 ↗
5. Cuntze RG. et al. Neue Bruchkriterien und Festigkeitsnachweise für unidirektionale Faserkunststoffverbunde unter mehrachsiger Beanspruchung—Modellbildung und Experimente. In: Fortschrittsberichte VDI, Vol. 5, No. 506, Düsseldorf: VDI Verlag, 1997.
6. Analysis of geometric imperfections affecting fibres in unidirectional composites10.1177/002199839603000403 ↗
7. A fatigue failure criterion for fiber reinforced materials10.1177/002199837300700404 ↗
8. Calculating 3D stresses in layered composite plates and shells10.1007/BF02257903 ↗