Hi everyone,
I'm searching some solution to absorb vibration. I'm trying to find materials and their properties to compare between them and chose one to design a vibration damper. Their application will be on the base of an avionics enclosure wich is onboard of a UAV (Unmanned Aerial Vehicle).
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Hi,
I observed that with
periodic boundary conditions on unit concrete unit cell, when uniaxial load is applied structure
behaves as if it is constrained to move in lateral direction, when
shear or other traction laoding is applied it has displacement
compatible behavior i.e, parallel edges has periodic deformation
behavior. With these above behavior can I conclude that for uniaxial
loading I need not apply periodic BCs and simply applying roller is
sufficient on lateral edges or there is no need to apply and periodic
BCs for uniaxial loading.
Dear imechanica user,
As i know, stresses existing in the components suffering no any outer forces are called the residual stresses. To reply the reason why the residual stress appears in the component?
Could anyone answer this question for my understanding.
regards,
Arefin
I'm having a hard time trying to relate the the forces specified in the figure so that I can obtain the expression for the strain energy release rate.
For the 'L-opening load' P when acting alone, the energy release rate is given by:
G= (12*P2*L2) / (E*B2*h3)
For the '2L/3-opening load' P when acting alone, the energy release rate is given by:
G=(16*P2*L2) / (3*E*B2*h3)
Through this post I wish to share some recent results that provide new insights into the role of a defect-core in mechanics. Below is the abstract of the work, and the references and links to the preprints of articles. I look forward to your comments and suggestions.
Abstract:
