Results 21 to 30 of about 16,028,301 (287)

Effects of post-heat treatment on microstructure, tensile properties, and bending properties of extruded AZ80 alloy

open access: yes, 2021
This study investigates the effects of post-heat treatments on microstructural characteristics, uniaxial tensile properties, and three-point bending properties of an extruded AZ80 alloy.
G. Lee, Jong-Un Lee, Sung Hyuk Park
semanticscholar   +1 more source

Micromagnetic studies of three-dimensional pyramidal shell-structures [PDF]

open access: yes, 2010
In this article we present a systematic, numerical analysis of the magnetic properties of pyramidal-shaped core-shell structures in a size range below 400nm.These are three dimensional structures consisting of a ferromagnetic shell which is grown on top ...
A Knittel   +17 more
core   +2 more sources

Numerical method for the prediction of bending properties of glass-epoxy composites [PDF]

open access: yesActa Periodica Technologica, 2007
Mechanical properties of composite materials are conditioned by their structure and depend on the characteristics of structural components. In this paper is presented a numerical model by which the bending properties can be predicted on the basis of ...
Stamenović Marina R.   +3 more
doaj   +1 more source

Influence of core spacing on bending properties of AlSi10Mg lattice sandwich panel formed by selective laser melting

open access: yesJournal of Aeronautical Materials, 2022
The light-weight and high-stiffness metal lattice sandwich structure formed by selective laser melting has an important application prospect in aerospace, military and other fields.
ZHANG Bo   +5 more
doaj   +1 more source

Influence of Extrusion Temperature on Properties of Graphene Oxide-Carbon Fiber/Epoxy Composite Prepared by Vacuum Infiltration Hot-Press-Forming Experimental System

open access: yesNanomaterials, 2022
Graphene oxide-carbon fiber/epoxy (GO-CF/EP) composites with extrusion temperatures of 30, 40, 50, 60 and 70 °C were prepared by a vacuum infiltration hot-press-forming experimental system (VIHPS).
Yuqin Ma   +6 more
doaj   +1 more source

Bending properties of extruded AZ91–0.9Ca–0.6Y alloy and their improvement through precompression and annealing

open access: yes, 2021
In this study, an extruded Mg–9Al–1Zn–0.3Mn–0.9Ca–0.6Y (AZXW9110) alloy is subjected to precompression and subsequent annealing (PCA) treatment for improving its bending formability, and the three-point bending properties of the as-extruded material and ...
Jong-Un Lee, G. Lee, Sung Hyuk Park
semanticscholar   +1 more source

Bending properties of structural foams manufactured in a hot press process

open access: yesAdvanced Manufacturing: Polymer & Composites Science, 2022
Thermoplastic foams allow manufacturing of lightweight parts with good thermal and acoustic insulation properties. To increase the mechanical properties without changing the part weight, these foams can be transformed into structural foams by a newly ...
Maximilian Salmins, Peter Mitschang
doaj   +1 more source

Comparison of Mechanical Properties According to the Structural Materials of Lumber, GLT, CLT, and Ply-lam CLT

open access: yesBioResources, 2023
The mechanical properties of materials such as lumber (L), glued laminated timber (GLT), cross-laminated timber (CLT), and Ply-lam CLT (P), which are laminated in cross layers, were compared.
Seungmin Yang   +4 more
doaj   +2 more sources

Mechanical Properties of Innovative, Multi-Layer Composite Laminated Panels

open access: yesBuildings, 2018
Cross-laminated timber (CLT) possesses both good shape stability and possible two-way force transfer ability due to its crosswise lamination. However, the transverse layers in CLT are prone to rolling shear failure under an out-of-plane load.
Jan Niederwestberg   +2 more
doaj   +1 more source

Bending properties and failure mechanism of fiber rare earth magnesium alloy super hybrid laminates

open access: yesJournal of Aeronautical Materials, 2021
The fiber metal laminate is mainly used in the fuselage wall board, wing skin and other key parts of the aircraft. The structural parts mentioned above bear a large bending moment during the service, which requires that the fiber metal laminate should ...
ZHAO Zong   +4 more
doaj   +1 more source

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