I am performing an FEA of a beam that is to be analyszed for maximum sagging under own weight...the purpose is to minimise the sagging by adding more supports...
analytical calculations considering two extreme end supports,i.e simply supported beam case revealed a maximum deflection of 17.5 mm...
i am trying to determine the maximum deflection of a beam on account of its sagging due to its own weight.
I have the CAD MODEL of the beam and i import its IGS into ANSYS WB14.static structural.
I performed analytical calculations considering uniformly distributed loading and simply supported...
I have a M20 bolt with 8.8 embossed on it and a nut with 5 embossed on it ..i seek to check the material of both these two by tightening them at the recommended torque(calculated by knowing the listed proof strength of bolt against 8.8 and yield strength of nut as per grade 6) .any thread...
The very thought of having a joint in seamless pipes seems absurd but what if the required length of seamless pipe is not available and the only option is to join two pipe pieces such that the joint sustains a particular operating pressure.?is welding recommended in this case?
The very thought of having a joint in seamless pipes seems absurd but what if the required length of seamless pipe is not available and the only option is to join two pipe pieces such that the joint sustains a particular operating pressure.?is welding recommended in this case?
The very thought of having a joint in seamless pipes seems absurd but what if the required length of seamless pipe is not available and the only option is to join two pipe pieces such that the joint sustains a particular operating pressure.?is welding recommended in this case?
Hello.
what exact relevance do strain gauges have in flexural testing of honeycomb sandwich panels ?
what particular property/variable can be calculated from the longitudinal strain data from the top and bottom face skins and how?location of strain gauges ?
we are primarily concerned about...
In my pursuit to obtain the properties for input to FEA of flexural behaviour of carbon fiber prepreg sandwich panel(aluminum core),I came across a research paper titled:
Fabrication, testing and analysis of composite sandwich beams by Isaac M. Daniel *, Jandro L. Abot
""The sandwich beam face...
Hello,
I am performing a bending test as per ASTM D7250 of a honeycomb sandwich panel comprising the following :
Face Skin
Material: carbon fiber epoxyPREPREG
Uni directional
1 skin consists of
[indent]3 plies of 0 degree
[indent]3 plies of 45 degree
[indent]3 plies of -45 degree
[indent]3...
Hello,
I am performing a bending test as per ASTM D7250 of a honeycomb sandwich panel comprising the following :
Face Skin
Material: carbon fiber epoxyPREPREG
Uni directional
1 skin consists of
[indent]3 plies of 0 degree
[indent]3 plies of 45 degree
[indent]3 plies of -45 degree
[indent]3...
Hello,
My facility has a wet sprinkler system that serves a shopping mall and a commercial building housing offices.the mall and the building share the same structure and the mall's basement houses the fire pumps.the building's basement is one level above the fire pump room's level and it here...
