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This standard determines the open-hole compressive strength of multidirectional polymer matrix composite laminates. The materials are restricted to continuous-fiber or discontinuous-fiber (tape or fabric) reinforced composites where the laminate is balanced and symmetric with respect to the test direction. The specimen geometry features a centrally located machined hole that acts as a controlled stress concentrator.
The specific width-to-diameter (W/D) and length-to-width (L/W) ratios are standardized to minimize edge effects and ensure a representative net-section failure mode across the hole centerline. The acceptable laminate thickness range is strictly controlled to prevent global buckling and ensure compatibility with the support fixture.
| 🟦 Parameter | 📏 SI Value | 📐 Inch-Pound Value |
|---|---|---|
| Specimen Width (W) | 38 mm | 1.5 in |
| Total Specimen Length (L) | 300 mm | 12.0 in |
| Hole Diameter (D) | 6.35 mm | 0.25 in |
| Laminate Thickness (t) | 2.0 to 5.0 mm | 0.080 to 0.200 in |
| Grip Length (each end) | 50 mm | 2.0 in |
The test method relies on a specialized U-shaped support fixture (described in Section 7.2 of the standard) that stabilizes the specimen against global buckling during compression loading. This fixture uses adjustable side supports and knife edges that contact the specimen edges, constraining lateral deflection while allowing free axial movement. It is referenced by several related standards including Practice D6742/D6742M (Filled-Hole), Practice D7615/D7615M (Open-Hole Fatigue), and Practice D8066/D8066M (Unnotched Compression).
The standard governs the test rate, conditioning environment, and number of replicate tests. Specimens must be loaded monotonically to failure while recording the maximum force.
| ⚙️ Parameter | 📏 Specification / Value |
|---|---|
| Test Speed (Crosshead) | 1.0 mm/min [0.05 in./min] |
| Standard Conditioning Atmosphere | 23 ± 3 °C [73 ± 5 °F] / 50 ± 10 % RH |
| Minimum Specimens per Condition | 5 (in accordance with Practice E122) |
| Primary Fixture Requirement | Anti-buckling support fixture (Sec. 7.2) |
The primary result of this test method is the Open-Hole Compressive (OHC) Strength, designated as Fcoh. This property quantifies the residual strength of a composite laminate in the presence of a standardized open hole under compressive loading.
The OHC strength is calculated using the net cross-sectional area of the specimen, which accounts for the reduction in area caused by the hole:
Fcoh = Pmax / (w × t – D × t)
Where:
Beyond strength, the standard requires the recording of the specific failure mode and location using the standard coding system (e.g., LGM, HGM, LAT). This data is essential for validating the quality of the test and for differentiating failure mechanisms between different material systems and laminates.
Open-Hole Compression (D6484) tests a laminate with an empty hole to measure the baseline notch sensitivity of the material. Filled-Hole Compression (Practice D6742/D6742M) places a fastener in the hole under either finger-tight or torqued conditions, which provides lateral support to the hole edge. This support typically yields a higher apparent strength compared to the open-hole configuration.
The standard width of 38 mm [1.5 in] and hole of 6.35 mm [0.25 in] provide a W/D of 6. This specific ratio is an industry standard designed to ensure that the stress concentration caused by the hole is not significantly influenced by the free edges of the specimen. It provides a clean, reproducible measurement of the notch sensitivity of the laminate system.
The most critical piece of specialized equipment is the compression support fixture (Sec. 7.2). Unlike standard compression test methods that use shear loading or end loading, this fixture provides lateral stability to the specimen face through side supports and knife edges to prevent global buckling over the unsupported gage section. This same fixture is shared by Practices D6742/D6742M, D7615/D7615M, and D8066/D8066M.
While the standard requires the laminate to be balanced and symmetric (Sec. 8.2.1), it does not prescribe a specific layup. Consequently, results (strength and failure mode) are highly dependent on the percentages of 0°, ±45°, and 90° plies. For standardized layups, D8509 (Guide for Test Method Selection and Test Specimen Design for Bolted Joint Related Properties) offers further guidance on designing laminates for specific quality control or design allowable generation programs.