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Titlebook: Mechanics of Composite, Hybrid and Multifunctional Materials, Fracture, Fatigue, Failure and Damage ; Proceedings of the 2 Vijay Chalivendr

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樓主: 婉言
41#
發(fā)表于 2025-3-28 18:01:43 | 只看該作者
H. M. Enginsoy,E. Bayraktar,F. Gatamorta,D. Katundi,I. Miskioglu
42#
發(fā)表于 2025-3-28 22:07:55 | 只看該作者
Vinicius L. Pereira,Isaías S. Almeida,Sabino A. Neto,Emin Bayraktar,Lygia P. Ferreira
43#
發(fā)表于 2025-3-28 23:55:37 | 只看該作者
Henriette Marlaine Imounga,Emilio Bastidas-Arteaga,Serge Ekomy Ango,Rostand Moutou Pitti
44#
發(fā)表于 2025-3-29 05:40:25 | 只看該作者
45#
發(fā)表于 2025-3-29 09:40:12 | 只看該作者
Conference proceedings 202221 SEM Annual Conference & Exposition on Experimental and Applied Mechanics, the third volume of four from the Conference, brings together contributions to this important area of research and engineering.? The collection presents early findings and case studies on a wide range of areas, including:.R
46#
發(fā)表于 2025-3-29 13:49:00 | 只看該作者
Flow Stress and Fracture Toughness Behavior of AA5083 Under Quasi-Static Loading,n rates (10. to 10./s) and flow stresses have been obtained for the corresponding strain rates. It is found that the aluminum alloy shows strain rate sensitivity in both tension and compression; however, this sensitivity was relatively more dominant in tension than in compression.
47#
發(fā)表于 2025-3-29 18:45:14 | 只看該作者
48#
發(fā)表于 2025-3-29 22:44:02 | 只看該作者
49#
發(fā)表于 2025-3-30 02:00:22 | 只看該作者
Mechanical Properties of Recycled Rubber Modified Epoxy Resin Based Composites for Aircraft Auxilia physical properties, .—Fracture toughness stress intensity factor and .—Critical energy release rate in mode I) have been determined by fracture toughness tests (static 3P bending test with single edge notch specimens, drop weight test, etc.).
50#
發(fā)表于 2025-3-30 04:03:29 | 只看該作者
Numerical Modeling of Recycled Rubber Based Composites Reinforced with Glass Fibers at High Strain mplemented for Finite Element Analysis Software ABAQUS/Standard as a user subroutine UMAT for implicit nonlinear finite element calculations in order to simulate the behavior of several RVEs representing the microstructure of the composite and it is behavior at high strain rates.
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