ASTM C273 Test Guide: Shear Testing for Composites
ShearAlways sandblast and solvent-wipe the steel loading plates to bare metal immediately before applying epoxy to prevent premature bond line…
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Always sandblast and solvent-wipe the steel loading plates to bare metal immediately before applying epoxy to prevent premature bond line…
Cure the bonded block assembly under a uniform dead-weight load to ensure a perfectly flat, parallel adhesive layer.
Grind the loaded ends of the sandwich panel flat and perpendicular to the facings within 0.02mm to eliminate edge stress…
Always use a direct-contact deflectometer setup to measure core deflection; crosshead travel includes platen-seating errors.
Always place the specified elastomer pads between the anvils and the panel to spread out high localized line loads.
Inspect specimens under a microscope post-test; you must verify that the failure was true interlaminar shear and not top-edge crushing.
Always bond back-to-back strain gauges on every specimen to actively compute and document real-time out-of-plane bending percentages.
You must gather both longitudinal and transverse strain simultaneously; in-plane shear strain equals axial strain minus transverse strain.
Always apply two cross-axial strain gauges mounted at $pm$45 degrees relative to the loading axis within the notch zone to…
Inspect the internal perimeter of the drilled hole under a microscope before testing; any evidence of fiber fraying or ply…
Meticulously measure the inner radius and thickness at the curved apex to ensure mathematical precision in out-of-plane stress conversions.
Calibrate the lever arm counterweight accurately prior to every setup to completely zero out dead-weight pre-loading.
Note that ASTM D7264 dictates a 32:1 span-to-thickness ratio, which is twice the 16:1 ratio specified by the plastics standard…