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 the stiffness values of the overal panel when testing as per ASTM D7250…
can strain gauges be done away with in favor of DIC{digital image correlation},given the constraint of having to install several gauges for a large number of test samples?
how much information can a DIC video camera provide for a given flexural test of a sample?be it 3-point or 4point?