ASTM D5961 simulates the joint conditions using bolt-loaded samples to determine how a composite laminate distributes the load and resists failure around fastener holes. Stress concentration around holes is introduced by fasteners in the composite material, so special importance must be given to studying realistic loading, with attention to the bearing behavior of the material. This is especially vital when it comes to validating designs for the aerospace and defense industries, where the design is intended to be exposed to demanding conditions using composite structures. The standard has several processes to suit different loading patterns and fastener patterns.
ASTM D5961 Test Method
| Specimen Preparation | Composite laminate specimens are machined to standard dimensions and drilled with one or more holes for fasteners. |
| Test Setup | Specimens are clamped and loaded using a tensile or compressive testing machine with the fastener(s) inserted. |
| Loading | Load is applied through the fastener, producing bearing stresses around the hole until failure or a specified strain limit is reached. |
| Data Acquisition | Load and displacement are recorded throughout the test. Some procedures also require the use of a strain gauge or extensometer. |
| Result Analysis | Key values such as ultimate bearing strength, offset bearing strength, and bearing strain are calculated. |
| Failure Mode Evaluation | The failure type, net tension, bearing, shear-out, or combined, is visually inspected and documented. |