Ben
I’m assuming that the strength and displacement columns are the raw data for your analysis . Will you tell us what units correspond to these values?
LOAD DATA IS IN LBS, BUT IT IS ONLY HALF THE ACTUAL LOAD. DISPLACEMENT IS MEASURED IN THREADS OF THE ACTUATOR. I CAN GIVE IT TO YOU IN INCHES WHEN I GET THE CHANCE TO MEASURE IT. THIS WILL ALL MAKE SENSE WHEN WE POST A VIDEO OF THE TEST METHOD.
I wonder if you can provide some additional insight to the failure modes for the various laminates.
THEY ALL FAILED BY BUCKLING. THE INTERESTING PART IS THE RATE AT WHICH BUCKLES PROPAGATED. WARP GLASS BUCKLED FASTER THAN YOU CAN SNAP YOUR FINGER. LAMINATES WITH 45DEG FIBERS BUCKLED SLOWER, LAMINATES WITH NYLON SKINZ BUCKLED EVEN SLOWER, AND LAMINATES WITH INNEGRA BUCKLED THE SLOWEST. THIS IS IMPORTANT IN UNDERSTANDING HOW MUCH ENERGY IS REQUIRED TO BREAK A SPECIMEN: TOUGHNESS. WHILE WARP GLASS MAY TAKE HIGHER LOADS, IT REQUIRES LESS ENERGY TO BREAK. THIS IS BECAUSE TOUGHER LAMINATES CAN REDISTRIBUTE THE LOAD PATH. THINK OF A GLASS WINDOW 1/16" THICK, AND A STEEL SHEET 1/16" THICK. GLASS IS STRONGER THAN STEEL, BUT STEEL IS MUCH MUCH TOUGHER. ALL YOU HAVE TO DO IS TAKE A TINY NAIL AND DRIVE IT INTO THE GLASS WINDOW, AND YOU WILL SEE CRACKS INSTANTLY PROPAGATE THROUGH THE ENTIRE WINDOW AND DESTROY THE WHOLE THING. DRIVE A NAIL THROUGH 1/16" STEEL PLATE AND YOU’LL ONLY GET A LITTLE HOLE…BECAUSE ALL THE ENERGY IS ABSORBED AND THE LOADS ARE REDISTRIBUTED.
In addition to sample geometry, you appear to use foam density and total sandwich weight as a control for most of the test. That said, this batch of data seems to be all about the layup
Was there any attempt to normalize the bend data based on the amount of fiber aligned with the principal bending stresses ?
THE GOAL OF THESE TESTS WAS TO ACHIEVE VARIABLE STIFFNESS LEVELS WITH SIMILAR RESISTANCE TO IMPACTS AND BUCKLING, AND SIMILAR WEIGHTS…AS THIS IS WHAT IS REQUIRED FOR MY FLEX TEST COMING SOON.
Others have already mentioned design based on fiber alignment with stress’ of interest.
Can I assume that only the 0 degree fibers (or cos( fiber angle)) contribute to bending strength in this test?
PAY CLOSE ATTENTION TO WHEN I USE THE TOUGH WORDS AND STRONG WORDS…THEY ARE CHOSEN DELIBERATELY AND SHOULD NOT BE INTERCHANGED.
TOUGHENING AND STRENGTHENING ARE TWO DIFFERENT THINGS FOR BOTH BENDING FAILURES AND IMPACT FAILURES. BENDING FAILURES (USUALLY BUCKLES) ARE CAUSED BY DESTABILIZATION OF THE SKIN DUE TO STRESSES IN ONE DIRECTION. IMPACTS GENERATE STRESS IN 360 DEG, BUT THEY WILL CRACK ACROSS THE LEAST TOUGH DIRECTION, WHICH HAPPENS TO BE THE STRONGEST DIRECTION…YES!!! CRACKS OF IMPACTS ARE FORMING PERPENDICULAR TO THE FIBER DIRECTION! EVEN THOUGH THE FIBERS ARE WHAT ADDS STRENGTH, THEY ALSO STIFFNESS SO THAT ALL THE LOADS ARE CARRIED BY THOSE FIBERS, AND THEY GET OVERLOADED. TO PREVENT IMPACTS, YOU SHOULD ADD MORE AXIS OF FIBERS SO THAT THE LOAD IS DISTRIBUTED MORE EVENLY IN ALL DIRECTIONS, A NICE BIPRODUCT OF THIS IS THAT THERE IS MORE INTERLAMINAR SHEAR…ABSORBING ENERGY. ALSO, ADDING A TOUGH FIBER LIKE SKINZ, POLYESTER CLOTH, INNEGRA, UHMWPE, OR KEVLAR WILL DO A LOT TO MITIGATE IMPACTS.
IDEALLY FOR SEVERE IMPACTS YOU HAVE A POLYMER CLOTH ON TOP AND BOTTOM OF GLASS.
IDEALLY FOR BUCKLE RESISTANCE AND MINOR IMPACTS (PRESSURE DINGS), YOU HAVE THE POLYMER CLOTH BETWEEN THE GLASS CLOTHS.
MY COMPROMISE IS THIS:
FOOT/ GLASS/ GLASS @45 / POLYMER/ FOAM CORE
OR
FOOT/ GLASS/ POLYMER/ GLASS @45 / FOAM CORE
IF YOU MESS AROUND WITH EITHER OF THESE LAYUP METHODS, YOU WILL BE VERY IMPRESSED.
What were the magnitudes of the impacts or how were the tests conducted?
THERE WILL BE A VIDEO SOON.
Regards,
-bill