ctan67
New member
- Oct 10, 2005
- 2
In regards to a bolted quasi-isotropic composite joint there are two failure modes that I am having questions about;
1)Bearing strength and
2)Fastener Pull-thru strength.
In MIL-HBK-17, I have come across text referring to bearing and pull-thru test procedures being used to determine the bearing and pull-thru responses of a composite.
Is there any type of micromechanics approach or method I can use to calculate such strengths knowing just the typical lamina tensile, comp, shear, moduli, strengths, etc?
The bearing load seems just like a compressive load on the interface, and my assumption was to simply calculate margins using the in-plane compressive strength of the laminate. How incorrect is this assumption?
The pull-thru strength is something I am a lot less familiar
with. My only grasp of this loading is that capacity seems to be dependent on thru-the-thickness properties. Can anyone please elaborate on what is going on mechanically and if there is at least a preliminary step I can take to figure out pull-thru strength before performing actual experimental tests?
Sidenote: Is there a hand calc equation for estimating pull-out stress?
1)Bearing strength and
2)Fastener Pull-thru strength.
In MIL-HBK-17, I have come across text referring to bearing and pull-thru test procedures being used to determine the bearing and pull-thru responses of a composite.
Is there any type of micromechanics approach or method I can use to calculate such strengths knowing just the typical lamina tensile, comp, shear, moduli, strengths, etc?
The bearing load seems just like a compressive load on the interface, and my assumption was to simply calculate margins using the in-plane compressive strength of the laminate. How incorrect is this assumption?
The pull-thru strength is something I am a lot less familiar
with. My only grasp of this loading is that capacity seems to be dependent on thru-the-thickness properties. Can anyone please elaborate on what is going on mechanically and if there is at least a preliminary step I can take to figure out pull-thru strength before performing actual experimental tests?
Sidenote: Is there a hand calc equation for estimating pull-out stress?