Information on the most widely used ASTM standards within the materials testing industry
ISO 14129 Composite In‑Plane Shear Property Tester | ±45° Tension Test | UnitedTest
ISO 14129 specifies the ±45° tension test method for fibre‑reinforced plastic composites to obtain in‑plane shear stress‑strain response, shear modulus and shear strength. UnitedTest manufactures ISO 14129 compliant universal testing machines for composite laminate mechanical characterization and quality certification.
ISO 14129 is an international standard for fibre‑reinforced plastic composites, describing the ±45° tension test method to determine in‑plane shear stress‑shear strain response, including key parameters of in‑plane shear modulus and in‑plane shear strength. A flat composite coupon with fibres oriented at +45° / −45° relative to the uniaxial loading direction is subjected to tensile pulling force. In‑plane shear behaviour of the laminate is back‑calculated from measured axial load data together with longitudinal and transverse strain readings.
This test setup does not apply pure shear load directly to specimens. Instead, the specially laid‑up ±45° composite laminate transforms axial tension force into a shear‑dominated material response along the principal material directions. Widely used for composite material R&D, laminate formulation screening, process optimization and incoming material inspection, ISO 14129 delivers critical shear performance data for aerospace, automotive, wind energy and industrial composite component validation.
UnitedTest develops and manufactures high‑precision ISO 14129‑compliant testing equipment for fibre‑reinforced plastic composites. Our test systems support accurate uniaxial tension loading and multi‑directional strain acquisition for ±45° composite coupons, generating repeatable in‑plane shear modulus and shear strength results for composite manufacturers, research laboratories and third‑party test institutions worldwide.
Test Principle
A rectangular flat laminate specimen with balanced‑symmetrical ±45° fibre orientation is subjected to uniaxial tensile loading. By measuring longitudinal strain (along specimen axis) and transverse strain (perpendicular to specimen axis), in‑plane shear strain is calculated as r12-ex-ey. In‑plane shear stress is derived from applied tensile force.
Important note: This loading condition does not produce pure shear, normal stress components still exist inside the laminate. Compared with ideal tube torsion test, this method tends to deliver lower ultimate shear strength and strain values. The test shall stop at shear strain r12=0.05(5 %) if specimen does not fracture earlier, to avoid errors caused by fibre rotation and temperature rise at large deformation.
Specific Test Method
It is the ±45° tension (off‑axis tensile) test for in‑plane shear property measurement:
1. Prepare balanced‑symmetric ±45n composite laminates;
2. Mount specimen into tensile grips, apply constant‑rate tensile displacement;
3. Continuously record tensile load, longitudinal strain and transverse strain;
4. Terminate test either at specimen fracture or at shear strain r12=0.05;
5. Compute in‑plane shear stress, shear strain, chord shear modulus G12 and in‑plane shear strength from recorded data.
Test Specimen Information
Geometry: Rectangular strip: total length = 250 mm, width = 25 ± 0.5 mm, nominal thickness = 2 ± 0.2 mm

Specimen quantity: Minimum 5 valid specimens. Specimens fractured within grips/tabs shall be discarded and retested
End tabs: 50 mm‑long end tabs are commonly bonded at both ends with high‑elongation adhesive (tab thickness: 0.5–2 mm, 90° non‑tapered geometry). Unbonded tabs or no tabs are allowed if failure does not occur inside grips.
Required Test Equipment of ISO 14129 In-Plane Shear Stress/Shear Strain Response Test
Complies with ISO 5893, force reading error less than ±1 % of full‑scale range, constant‑crosshead‑speed control capability. Grips for flat composite coupons. | |
Strain measurement system | Strain gauges or extensometers, accuracy within ±1 % full‑scale, to capture both axial and transverse strains on specimen gauge section. |
Auxiliary Accessories | Cutting/machining tools for composite panels, high‑elongation adhesive for bonding end tabs, coolant for specimen machining to avoid heat accumulation. |
Main Test Parameters
| Standard crosshead speed | 2 mm/min (if material specification does not specify) |
| Termination shear strain limit | =0.05 (5 %) |
| Modulus calculation strain window | |
| Dimension measurement precision | width: 0.1 mm; thickness: 0.02 mm |
| Conditioning & test atmosphere | Follow ISO 291 when no material‑specific requirement exists |
| Reporting precision | Stress and modulus values to three significant figures |
Adhesive for end tabs shall have high elongation, shear strength > 30 MPa, higher elongation than the tested composite material.
Test Procedures of ISO 14129 In-Plane Shear Stress/Shear Strain Response Test
1. Fabricate composite panel following ISO 1268 or agreed procedure with balanced‑symmetric ±45° lay‑up. Machine specimens complying with ISO 2818, apply end tabs if required.
2. Inspect geometry and surface quality, reject defective specimens.
3. Perform conditioning according to ISO 291 or material specification.
4. Measure specimen width and thickness at specimen mid‑point.
5. Mount strain gauges / extensometers along and perpendicular to specimen axis.
6. Install specimen into test machine grips, set cross‑head speed (normally 2 mm/min).
7. Continuously collect tensile force, longitudinal and transverse strain data throughout loading.
8. Stop test when specimen fractures OR shear strain reaches 0.05. Record failure load and failure mode. Discard results for grip‑region fracture.
9. Calculate shear stress‑strain curves, G12 modulus and shear strength for each valid replicate. Compute arithmetic mean, standard deviation and 95 % confidence interval as required.
Industry Application Fields
This test characterizes in‑plane shear behaviour of fibre‑reinforced polymer laminates, widely used in:
Aerospace: qualification of carbon‑fibre composite laminates for aircraft structures;
Automotive: composite component material development for lightweight vehicles;
Wind‑energy: mechanical property evaluation of wind‑turbine blade composite materials;
General composite R&D, material batch acceptance, laminate formulation comparison for thermoset and thermoplastic FRP laminates (unidirectional‑ply or woven‑fabric laminates, excluding coarse fabrics).
Related Standard:
| ASTM D5379 | Standard Test Method for Shear Properties of Composite Materials by the V-Notched Beam Method |
| GOST R 57968 | Polymer composites. Test method of samples for shearing |
| ISO 14129 | Fibre-reinforced plastic composites - Determination of the in-plane shear stress/shear strain response, including the in-plane shear modulus and strength, by the ˝45° tension test method |
| ASTM D3518 | Standard Test Method for In-Plane Shear Response of Polymer Matrix Composite Materials by Tensile Test of a ±45° Laminate |
| ASTM D7078 | Standard Test Method for Shear Properties of Composite Materials by V-Notched Rail Shear Method |
| ISO 14130 | short‑beam interlaminar‑shear test |
| GB/T 28889 | Test method for in-plane shear properties of composite materials |
| ISO 527‑5 | Tensile‑property standard for unidirectional fibre‑reinforced plastics. ISO 14129 harmonises document format, specimen‑size rules and modulus‑measurement strain references with ISO 527‑5 |
| ASTM D4255 | Standard Test Method for In-Plane Shear Properties of Polymer Matrix Composite Materials by the Rail Shear Method |
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Related products and device
Related Standard
ASTM D5379 Standard Test Method for Shear Properties of Composite Materials by the V-Notched Beam Method
ASTM D5379 used for characterizing the shear behavior of advanced fiber‑reinforced composites. Often referred to as the Iosipescu shear test. It quantifies both in-plane shear (1-2 plane) and interlaminar shear (1-3, 2-3 planes) of fiber-reinforced polymer composites, covering continuous unidirectional laminates, woven fabric laminates, balanced symmetric panels, and random short-fiber molded composites (SMC). This testing method measures shear stress/strain, ultimate strength and strain, as well as shear string elastic modulus.
ASTM D7078 V‑Notched Rail Shear Test for Composite Materials
ASTM D7078 determines shear properties of high‑modulus fibre‑reinforced composite materials by clamping a V‑notched specimen between two pairs of loading rails and pulling the rails in tension. The rails transmit shear forces through the faces of the specimen (face‑loading), which allows higher shear forces to be applied than in edge‑loaded methods.
ASTM D4255 Standard Test Method for In-Plane Shear Properties of Polymer Matrix Composite Materials by the Rail Shear Method
ASTM D4255 is a test method for testing the in-plane shear properties of high-modulus fiber-reinforced composite materials. The method is divided into two procedures. Procedure A tests laminates clamped between two pairs of loading rails. When loaded in tension the rails introduce shear forces in the specimen. In Procedure B, laminates clamped on opposite edges with a tensile or compressive force applied to a third pair of rails in the center are tested.
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.
FAQs about ISO 14129 (±45° Tension Shear Test)
Q1: What is ISO 14129 test?
A1: ISO 14129:1997 is an international standard for fibre‑reinforced plastic composites. It uses the ±45° tension test to measure in‑plane shear stress‑strain response, in‑plane shear modulus G12 and in‑plane shear strength T12M of balanced‑symmetric composite laminates.
Q2: Why is ISO 14129 test important for composite materials?
A2: In‑plane shear properties are core input data for FEA simulation and laminate structural design. Shear behaviour reflects matrix performance and fibre‑matrix interface quality. Compared with complex tube‑torsion pure‑shear tests, ISO 14129 uses simple flat specimens and common universal tensile testers, suitable for R&D, batch quality control and material‑to‑material comparison across labs. It captures the full nonlinear shear stress‑strain curve, not only single‑point modulus/strength values.
Q3: Which materials are suitable for ISO 14129 test? Are there material limitations?
A3: Suitable for thermoset and thermoplastic matrix laminates made from unidirectional plies or woven fabrics, with balanced‑symmetric ±45° lay‑up.
Not suitable for coarse fabrics. Test results are sensitive to ply quantity and ply distribution; always use identical ply count for material comparison.
Q4: What is the difference between ISO 14129 and ASTM D3518?
A4: Both implement ±45° tensile in‑plane‑shear test and share the same 5 % shear‑strain failure criterion. ISO 14129 is European‑origin ISO standard; ASTM D3518 is US‑origin standard. There are minor differences in specimen‑preparation notes and report‑item requirements. Test data from the two standards cannot be directly mixed for comparison without validation.
Q5: Can ordinary universal tensile machine perform ISO 14129 test?
A5: Yes, but the machine must meet three key requirements: high‑frame alignment accuracy, stable constant‑crosshead‑speed control (standard speed 2 mm/min), and capable to receive external strain‑gauge / extensometer signals. Displacement‑only reading cannot substitute direct strain measurement for ISO 14129 modulus calculation.
Q6. Why use a ±45° tensile specimen instead of a pure shear test?
A6: A ±45° laminate converts axial tension into a shear-dominated state in the material’s 1–2 direction. It is simpler, cheaper, and uses a standard universal testing machine—no special shear fixture required.
Q7. Is ISO 14129 good for shear modulus or shear strength?
A7: It is reliable for shear modulus. For ultimate shear strength, results can be conservative for high-shear-elongation materials because fibre rotation, heating, and flat load–strain behaviour make true failure hard to define. That’s why the test stops at γ₁₂ = 0.05 if no failure occurs.
Q8. Can UnitedTest machines perform ISO 14129?
A8: Yes. UnitedTest can supply universal tensile testing machines, composite grips, extensometers / strain gauge systems, and custom fixtures configured for ISO 14129, ASTM D3518, ISO 527-5, and other FRP standards.
Q9: Why choose ISO 14129 ±45° Composite Shear Testing Machine — by UnitedTest?
A9: UnitedTest supplies ISO 14129 compliant universal testing machines for fibre‑reinforced plastic composite ±45° tension in‑plane shear test, measuring shear modulus G12 and shear strength.
ISO 14129 Universal Testing Machine for Fibre‑Reinforced Plastic Composites
UnitedTest is a professional manufacturer of material testing machines, providing complete test solutions for ISO 14129:1997‑ ±45° tension test to determine composite in‑plane shear stress‑strain response, shear modulus and shear strength by UnitedTest.
Our universal testing machines (WDW‑series electromechanical UTM, hydraulic UTM models) fully satisfy ISO 14129 requirements for fibre‑reinforced thermoset and thermoplastic composite laminates. It obtains key composite material parameters: in‑plane shear modulus G12, in‑plane shear strength T12M, and full shear‑stress‑shear‑strain curves for balanced‑symmetric ±45° composite specimens.
✅ Core machine capabilities for ISO 14129 test:
- High‑stiffness test frame with excellent alignment performance, conforming to ISO 5893 machine requirement;
- Force measurement accuracy ≤ ±1 % full‑scale; supports constant cross‑head speed setting (standard 2 mm/min);
- Compatible with strain‑gauge signal acquisition and contact‑type / non‑contact extensometer;
- Test software pre‑integrates ISO 14129 calculation formulas: shear stress, shear strain, chord shear modulus G12 calculation;
- Automatically generates complete ISO‑standard test reports including mean value, standard deviation, confidence interval and failure‑mode record;
- Supports wedge grips, hydraulic tensile grips and custom fixture accessories for composite laminate specimens;
- Covers load range 5 kN ~ 300 kN for different carbon‑fibre / glass‑fibre composite material gradesUnitedTest.
This ISO 14129 ±45° in‑plane shear test solution is widely adopted in aerospace composite R&D, automotive lightweight composite development, wind‑turbine‑blade material quality control, composite‑lab material characterisation and incoming‑material inspection.
UnitedTest testing machines also support correlated composite standards: ASTM D3518, ISO 527‑5, ISO 14130 and other polymer‑composite test standards. If you need specimen‑preparation guidance, fixture selection advice or quotation for ISO 14129 composite‑shear‑test system, please contact our engineering team.
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