Theoretical solution for Impact response of FML(Fibre-metal lamiantes)
A theoretical solution for Impact response of FML(Fibre-metal lamiantes) is available:
Low-velocity impact response of fiber-metal laminates – A theoretical approach
A theoretical solution for Impact response of FML(Fibre-metal lamiantes) is available:
Low-velocity impact response of fiber-metal laminates – A theoretical approach
Dear all,
A paper on the Low-Velocity Impact Response and failure characteriztion of Fibre-Metal Laminates – Experimental and Finite Element Analysis, has been issued by
http://www.sciencedirect.com/science/article/pii/S0266353812002850
Authors:Shengqing Zhu & Gin Boay Chai
Dear all,
Can anybody give me some papers on the grain size T3 2024?
I know it should be 10-100 μm or so. But I want to get a more precise data and cite it in my journal paper.
All suggestion or papers are welcome. Thanks.
Dear All,
I am presently deducting formula for a metallic circular plate with large deflection. Can anybody help me how to dedcut the membrane strain energy of a circular plate?
All information on reference or textbook are all welcome.
Thanks.
Jason
Dear all,
I am trying to apply the Yield line theory to analyze the fracture of a disk by central load, F.
Do anybody know the yield line on the disk? I searched some books to find most references focus on rectangular plate rather than disk.
All suggestions are welcome. Thanks.
Dear all,
I will model a bird to impact a shell at high velocity by ABAQUS. I decide to model the "bird" by ALE mesh and referred by EOS equation.
However, most simulation works are done by LS-Dyna. Do anyone know how to determine the parameters in ABAQUS for the "bird" in EOS equation?
All suggestions are welcome.
Thanks.
Jason,
Best regards