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ASTM D5766 open-hole tensile test for composite laminates

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ASTM D5766 Open Hole Tensile Tester | Composite Laminate OHT Testing | UnitedTest

ASTM D5766 standard tests open-hole tensile strength (OHT) of multidirectional fiber-reinforced polymer composite laminates, simulating structural fastener cut-out notch effects. UnitedTest manufactures ASTM D5766 compliant notched composite tensile testing machines for aerospace structural quality control.


ASTM D5766 is a key standardized test method dedicated to evaluating the open-hole tensile strength (OHT), also known as notched tensile strength, of multi-directional fiber-reinforced polymer matrix composite laminates. Built upon the classic ASTM D3039 tensile testing framework, this method uses standard tensile coupons with a precision-machined central through-hole, loaded under uniaxial tension until structural failure occurs.

This test effectively quantifies the notch sensitivity and stress concentration effect caused by central perforations on composite laminates. It accurately simulates real-world fastener cut-outs, drilling holes and structural cutaway features widely applied in aerospace, automotive and wind energy composite structures. ASTM D5766 test data provides critical performance parameters for structural design safety verification, damage tolerance evaluation, composite material qualification and batch production quality inspection.


UnitedTest designs and manufactures high-precision ASTM D5766 open-hole tensile testing machines fully compliant with standard test specifications. Our professional composite test equipment delivers stable uniaxial tension loading, precise failure data recording and repeatable OHT test results, ideal for advanced composite laboratories, aviation material R&D institutions and industrial structural component certification.


Test Principles: 

A balanced, symmetric multi‑directional laminate coupon containing a centrally located circular hole is loaded in uniaxial tension to failure, following the apparatus, alignment and procedure rules of ASTM D3039/D3039M.

The key conceptual point: the hole creates a stress concentration and a reduced net section, and the resulting failure is governed by that notch. Strength is nevertheless reported on the gross cross‑sectional area (w × h), deliberately ignoring the hole . This is an aerospace design convention: it folds the effect of the notch into the strength number itself so the value can be used directly as a notched design allowable (a "remote stress") without re‑computing stress concentrations for fastener holes, free edges, flaws or damage not explicitly modelled in the stress analysis .

The only acceptable failure mode is one that passes through the hole. Anything else is invalid data.

ASTM D5766 open-hole tensile test for composite laminates


Test Specimen information

LaminateMulti‑directional, balanced and symmetric about the test direction; fibers in ≥2 directions; continuous‑fiber or discontinuous‑fiber (tape and/or fabric)
Standard lay‑up

Typically [45ᵢ/−45ⱼ/0ⱼ/90ₖ]ms tape or [45ᵢ/0ⱼ]ms fabric, with ≥5 % of fibers in each of the four principal orientations — this family gives the highest likelihood of acceptable failure modes. Not suitable for unidirectional (single‑orientation) tape laminates.

ASTM D5766 open-hole tensile test for composite laminates

ThicknessNominal 2.5 mm [0.10 in.], permissible 2–4 mm [0.080–0.160 in.]
Width36 ± 1 mm [1.50 ± 0.05 in.] (both configurations)
LengthConfig. A: 200–300 mm [8–12 in.] (preferred, general lay‑ups); Config. B: 150–200 mm [6–8 in.] (limited to quasi‑isotropic lay‑ups, grip length 35–55 mm, ungripped length ≥75 mm)
HoleCentral, 6.00 ± 0.06 mm [0.250 ± 0.003 in.] diameter; centered along length to within 0.12 mm [0.005 in.] and across width to within 0.05 mm [0.002 in.]
TabsOptional; generally not needed — the hole is a sufficient stress riser to force failure in the notched region
Hole preparationDrill undersized then ream to final size; must not delaminate or otherwise damage material around the hole. Backing the laminate with a sacrificial board and using composite‑specific drills are standard shop practice. Method must be recorded and reported.
Key ratiosw/D = 6 (maintain unless the study is about this ratio); D/h preferred 1.5–3.0 


Test Equipment required of ASTM D5766 open-hole tensile test for composite laminates

Universal testing machine

Conforms to ASTM D3039/D3039M requirements, capable of controlled constant cross‑head speed, continuous force‑displacement recording. 

Micrometer or gauge

capable of measuring hole diameter to ±0.025 mm [±0.001 in.] — an explicit additional requirement beyond D3039 .

Edge‑mounted extensometer

Installed on specimen edges across the hole gage section, used to capture local strain response and compute percent bending of the coupon.

Specimen machining toolsUndersize drill + reamer for hole fabrication (to avoid hole‑edge delamination damage)
Temperature chamberfor non‑ambient testing (electric heating, CO₂ or LN₂ cooling), plus thermocouples.


Test parameters and stipulations

Speed: in practice ≈2 mm/min crosshead rate (chosen so failure occurs in roughly 1–10 min)

Sampling rate: 2–3 Hz, ≥100 points/test.

Dimensional measurements: Measure actual hole diameter D, specimen width w, thickness h


Step-by-Step Test Procedure of ASTM D5766 open-hole tensile test for composite laminates

  1. Pre‑test preparation: Confirm sampling method, specimen geometry, conditioning scheme, extensometer requirements, and target test parameters. Measure width, thickness, and precisely measure hole diameter; inspect hole edges for delamination damage.

  2. Environmental conditioning (if specified): Condition specimens per D5229/D5229M and keep specimens in conditioning environment until test execution; document moisture content and exposure parameters.

  3. Mount specimen in tensile machine: Align specimen axially; fit edge‑mounted extensometers across the hole gage section if strain measurement is needed.

  4. Conduct tensile test: Run monotonic tensile loading following D3039/D3039M procedure. Continuously record force‑crosshead‑displacement (and force‑strain with extensometer). Capture force at initial damage events, maximum force, rupture‑point displacement.

  5. Post‑test inspection: Record three‑character failure‑mode code for each specimen. Discard results for coupons failing outside the hole gage‑middle zone and perform retest.

  6. Data computation: Calculate open‑hole tensile strength, actual w/D, actual D/h, sample average, standard deviation and CV. Report values to three significant figures where required.


Industry applications

Aerospace & defense (the primary driver): notched design allowables for wing/fuselage skins, covers, frames and control surfaces; bolted‑joint bearing/bypass analysis; material qualification and specifications; quality assurance / batch acceptance .

Automotive & motorsport: carbon‑fiber structures with mechanically fastened joints or cut‑outs.

Wind energy: blade root and structural laminates with holes/cut‑outs.

Marine, rail, infrastructure: composite panels and joints in harsh environments.

R&D and material development: quantifying notch sensitivity, comparing lay‑ups, fiber/matrix systems, drilling processes and toughening strategies; validating progressive‑damage FE models.

Data generated with this method feeds CMH‑17 (Vol. 1 Ch. 2 material characterization; Vol. 3 Ch. 11 bolted joints; Ch. 12 damage‑tolerance allowables) databases .


Related Standard:

ISO 527‑4 / ISO 527‑5

tensile properties of isotropic and orthotropic fiber-reinforced plastic composites.

tensile properties of unidirectional fiber-reinforced composites. These are the nearest ISO counterparts; a formal ASTM/ISO harmonization study exists, but specimen dimensions, grip recommendations and the modulus chord differ.

ASTM D3039Standard Test Method for Tensile Properties of Polymer Matrix Composite Materials
GB/T 3354

Test method for tensile properties of orientation fiber reinforced polymer matrix composite materials

EN 2561 / EN 2597European aerospace series CFRP unidirectional laminate tensile test parallel (and transverse) to the fiber direction.
SACMA SRM 4R-94Legacy industry method, historically used alongside early D3039 editions
ASTM D3479tension–tension fatigue; explicitly uses the D3039 specimen geometry.
ASTM D5766
open-hole (notched) tensile strength.
ASTM D6484Open‑Hole Compressive Strength
ASTM D6742Filled‑Hole Tension & Compression Practice
ASTM D7291through-thickness ("flatwise") tensile strength and modulus.
ASTM D3518in-plane shear response by tensile test of a ±45° laminate; same straight-sided coupon, no fixture.


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ASTM D5766 Composite laminates open-hole Tensile Testing Machine

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Related Standard

ISO 527-4, ISO 527-5 Tensile Test on fibre-reinforced Composites –

ISO 527-4 and ISO 527-5 are two key standards within the ISO 527 series for determining the tensile properties of fibre-reinforced plastic composites. 

ISO 527-4 covers the general principles and tests for isotropic and orthotropic materials. ISO 527-5 provides specific procedures for testing unidirectional fiber-reinforced composites.


These standards are critically important because they provide a unified, reliable method to measure fundamental mechanical properties (like tensile strength, modulus, and strain) which are essential for material selection, quality control, structural design, and R&D in aerospace, automotive, wind energy, and sports equipment industries.


ISO 527-3 Tensile Test on Plastic Film –

ISO 527-3 Plastics - TENSILE PROPERTIES - PART 3: FOR FILMS AND SHEETS

ISO 527-3 specifies the test conditions for determining the tensile properties of plastic films and sheets with a thickness less than 1 mm, based on the general principles of ISO 527-1. Provides standardized procedures to measure critical mechanical parameters including tensile strength, yield strength, elongation at break, and Young's modulus for thin plastic materials. It is critically important because thin films behave very differently under stress compared to rigid plastics; they are more prone to tearing, slipping, and deformation. By standardizing the test conditions, this document ensures that material specifications, quality control, and research data are globally comparable and reliable.  Specimen created following ISO 527-3 can be used to determine the tensile properties of thin plastic sheets and films including the tensile modulus of elasticity and the tensile energy to break (TEB).

ISO 527-1, ISO 527-2 Tensile Test of Plastics Composites & plastics –

ISO 527-1 covers the test procedures for determining tensile properties of plastics and plastic composites. Tensile properties of plastics that are determined through the practices of ISO 527-1 include tensile strength, tensile modulus and other properties related to stress strain characteristics of plastic materials. 

ISO 527-2 specifies the test conditions for determining the tensile properties of moulding and extrusion plastics, based upon the general principles given in ISO 527-1. The methods described in ISO 527-2 are selectively suitable for use with the following range of materials: rigid and semi-rigid thermoplastics moulding, extrusion and cast materials, including compounds filled and reinforced by, for example, short fibres, small rods, plates or granules but excluding textile fibres (see ISO 527-4 and ISO 527-5).

ASTM D882 Tensile test of Thin Plastic Sheeting –

ASTM D882: Standard Test Method for Tensile Properties of Thin Plastic Sheeting

ASTM D882 designed to measure tensile mechanical properties including ultimate tensile strength, yield strength, elongation, tensile energy to break and tensile modulus of elasticity of thin plastic films and sheeting with thickness below 1.0 mm (0.04 in.) It covers full testing workflows including specimen preparation, conditioning, equipment configuration, tension loading, data recording, mathematical calculation, and result reporting for flexible thin plastic substrates. The samples are cut in strips that minimally have to be eight times longer than wide. No dumbbell shape is cut for materials of that thickness. Cut samples need to be free of nicks and other cutting defects since they will have an important impact on the test results variation. 

ASTM D638 Tensile Testing for Plastics –

ASTM D638 determining the tensile properties of unreinforced and reinforced plastics using dumbbell-shaped (dogbone) specimens tested under closely controlled conditions of conditioning, temperature, humidity, and crosshead speed. For measuring the tensile mechanical properties of unreinforced and reinforced plastics, including thermoplastics, thermosets, molded plastics, and plastic composites.

ASTM D3039 Tensile Testing of Polymer Composites –

ASTM D3039 Standard Test Method for Tensile Properties of Polymer Matrix Composite Materials

ASTM D3039 defines a unified procedure to measure the in-plane tensile properties of high-modulus fiber-reinforced polymer matrix composites (PMC). It applies exclusively to continuous or discontinuous fiber-reinforced laminates that are balanced and symmetric with respect to the test direction.  

ASTM D5766 Open‑Hole Tensile Test FAQs

Q1: What is ASTM D5766 test used for?

A1: ASTM D5766 measures open‑hole tensile strength (OHT) of balanced‑symmetric multi‑directional polymer‑matrix composite laminates. It evaluates tensile performance weakened by a central drilled hole, simulating fastener holes, cut‑outs or access openings found in real composite structural parts.


Q2: Why is ASTM D5766 test important for composite materials?

A2: Composite laminates are highly notch‑sensitive, without metal‑like plastic yielding to relieve stress concentration around holes. Un‑notched tensile results (ASTM D3039) overestimate real‑world component capacity. D5766 generates reliable notched design allowables for aerospace, automotive composite structural sizing, material qualification and laminate lay‑up optimization. It also reflects hole‑drilling manufacturing quality via test strength variation.


Q3: What are valid failure modes for ASTM D5766 test? When should I discard test data?

A3: Only three valid three‑place failure‑mode codes are allowed: LGM (Lateral‑Gauge‑Middle), AGM (Angled‑Gauge‑Middle), MGM (Multi‑mode‑Gauge‑Middle). Failure must occur in the gauge‑middle zone right at the open hole. If fracture appears in grip region or away from the central hole, the test result is invalid and retest is required, unless studying pre‑existing flaws intentionally.


Q4: What are Configuration A and Configuration B specimens? What is difference?

A4:

  • Configuration A (preferred general‑purpose): Specimen length 200‑300 mm, for most balanced‑symmetric multi‑directional laminates. Long enough to build uniform strain field outside hole‑influence area.

  • Configuration B: Specimen length 150‑200 mm, limited only to quasi‑isotropic stacking sequences. Minimum un‑gripped length ≥75 mm to avoid grip‑boundary effect on hole‑zone failure. Both versions share nominal width = 36 mm, hole diameter = 6 mm, nominal w/D ratio = 6.


Q5: Why keep w/D (width‑to‑hole‑diameter) ratio =6 in ASTM D5766?

A5: Stress distribution near the hole interacts with specimen side edges. Fixed w/D=6 minimizes edge‑interference effect and creates comparable stress concentration state, so test data from different laboratories and specimen batches can be directly compared. Both nominal ratio and measured actual ratio must be reported to three significant figures in final report.


Q6: Do I need bonded tabs for ASTM D5766 test coupons?

A6: Tabs are optional and generally not required. The central hole acts as strong stress riser to force failure within hole gauge‑middle area. Tabs can still be applied if you encounter premature grip‑area damage, but it is not mandatory per the standard.


Q7: Can I directly use ASTM D3039 un‑notched tensile strength for composite parts with bolt holes?

A7: No. It is a risky shortcut in composite design. The open hole produces heavy strength reduction by stress concentration. Real composite structures with fastener holes must use open‑hole tensile allowables generated from D5766 rather than un‑notched D3039 values for structural safety design.


Q8. What is the difference between ASTM D5766 and ASTM D3039?

A8: D3039 measures unnotched tensile properties and is the base method D5766 refers to for apparatus, geometry, alignment and procedure. D5766 adds the hole and yields a notched allowable. Unnotched data is for basic material characterisation; OHT data is what structures containing holes are sized on. They are complementary, never interchangeable — OHT is commonly 40–50 % below unnotched strength for quasi‑isotropic CFRP/GFRP.


Q9. How does UnitedTest support ASTM D5766 testing?

A9: UnitedTest supplies electromechanical and hydraulic universal testing machines with the force accuracy (ISO 7500‑1 Class 0.5/1, ASTM E4), stepless speed control and gripping needed for D5766, plus wedge and pneumatic grips, compression platens, extensometers, environmental chambers and fixtures built to ISO, ASTM, EN and DIN requirements. SmartTest software lets you build a D5766 method with gross‑area strength calculation, w/D and D/h ratios, failure‑code entry and automatic mean, standard deviation and CV statistics, then generate a compliant report. Send UnitedTest your material, lay‑up, coupon size and expected failure load, and the team will specify the frame, load cell, grips, extensometer and chamber for your application.


Q10: Why choose ASTM D5766 Open‑Hole Tensile Testing Machine from UnitedTest?

A10: UnitedTest manufactures high‑performance universal testing machines fully compliant with ASTM D5766/D5766M‑23 standard for open‑hole tensile strength test of polymer‑matrix composite laminates. Suitable for CFRP, GFRP tape & fabric composite coupons for aerospace, automotive composite material qualification, R&D and quality control. Complete test fixtures, precision extensometer and dedicated composite test software available.


UnitedTest is a professional manufacturer of material testing equipment supplying complete solutions for ASTM D5766/D5766M‑23 open‑hole tensile strength test for polymer‑matrix composite laminates.

Our universal tensile test system performs standard open‑hole tension test for multi‑directional balanced‑symmetric composite laminates (continuous‑fiber tape, fabric or discontinuous‑fiber reinforced composites). It simulates real‑world stress concentration around fastener holes and cut‑outs, measuring open‑hole tensile strength (OHT) for composite material screening, structural design allowable generation, incoming‑material QC and aerospace‑grade composite qualification.


✅ Full compliance with ASTM D5766‑23 requirements

  • Compatible with both Configuration A and Configuration B specimen geometries

  • High‑accuracy load‑cell, stable cross‑head speed control following ASTM D3039 baseline requirements

  • Supports edge‑mounted extensometer for local strain measurement and percent‑bending calculation

  • Dedicated composite test software: auto‑calculates OHT strength, w/D ratio, D/h ratio, mean value, standard deviation and CV coefficient of variation; supports recording LGM / AGM / MGM failure‑mode codes; exports complete D5766‑compliant test reports.

  • Optional customized test fixtures, anti‑slip wedge grips, micrometer accessories for hole‑diameter inspection.

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