ASTM E1922/E1922M-22 PDF
Standard Test Method for Translaminar Fracture Toughness of Laminated and Pultruded Polymer Matrix Composite Materials
Standard Test Method for Translaminar Fracture Toughness of Laminated and Pultruded Polymer Matrix Composite Materials
- Статус документа:
- Действующий
- Формат:
- Электронный (PDF)
- Количество страниц:
- 8
- Дата публикации:
- 1 мая 2022 г.
- Издание:
- E1922/E1922M
- ICS:
- 83.140.20
SIGNIFICANCE AND USE 5.1 The parameter KTL determined by this test method is a measure of the resistance of a polymer matrix composite laminate to notch-tip damage and effective translaminar crack growth under opening mode loading. The result is valid only for conditions in which the damage zone at the notch tip is small compared with the notch length and the in-plane specimen dimensions. Alternately, for materials exhibiting distributed damage in a larger volume, observed force-displacement and discrete damage events are still valid structural responses for certain specific engineering applications. 5.2 This test method can serve the following purposes. In research and development, (a) KTL data can quantitatively establish the effects of fiber and matrix variables and stacking sequence of the laminate on the translaminar fracture resistance of composite laminates; and (b) quantified distributed damage measurements can be used to validate progressive composite damage models. In structural design, KTL data can, within the constraints of the specimen geometry and loading, be used to assess composite laminate resistance to damage growth from edge flaws and notches. 5.3 The translaminar fracture toughness, KTL, as well as distributed damage observations, determined by this test method may be a function of the testing speed and temperature. This test method is intended for room temperature and quasi-static conditions, but it can apply to other test conditions provided that the requirements of 13.2 and 13.3 are met. Application of KTL in the design of service components should be made with awareness that the test parameters specified by this test may differ from service conditions, possibly resulting in a different material response than that seen in service. Distributed damage observations are also limited to the material and geometry tested, but may be more generally applied to a variety of structural analysis validation applications. 5.4 Not all types of laminated polymer matrix... SCOPE 1.1 This test method covers the determination of translaminar fracture toughness, KTL, for laminated, molded, or pultruded polymer matrix composite materials of various fiber orientations using test results from monotonically loaded notched specimens. If the material response is such that the KTL calculation is not valid, alternate reporting methods are provided. 1.2 This test method is applicable to room temperature laboratory air environments. 1.3 Composite materials that can be tested by this test method are not limited by thickness or by type of polymer matrix or fiber, provided that the specimen sizes and the test results meet the requirements of this test method. This test method was developed primarily from test results of various carbon fiber – epoxy matrix laminates and from additional results of glass fiber – epoxy matrix, glass fiber-polyester matrix pultrusions and carbon fiber – bismaleimide matrix laminates (1-4, 5, 6).2 1.4 A range of eccentrically loaded, single-edge-notch tension, ESE(T), specimen sizes with proportional planar dimensions is provided, but planar size may be variable and adjusted, with associated changes in the applied test load. Specimen thickness is a variable, independent of planar size. 1.5 Specimen configurations other than those contained in this test method may be used. It is particularly important that the requirements discussed in 5.1 and 5.4 regarding contained notch-tip damage be met when using alternative specimen configurations in conjunction with the KTL calculation. 1.6 Units—The values stated in either SI units or inch-pound units are to be regarded separately as standard. The values stated in each system are not necessarily exact equivalents; therefore, to ensure conformance with the standard, each system shall be used independently of the other, and values from the two systems shall not be combined. 1.6.1 Within the text, the inch-pound units are shown ...
Abstract
Overview
ASTM E1922/E1922M-22 establishes a standard test method for determining the translaminar fracture toughness (KTL) of laminated and pultruded polymer matrix composite materials. This method is integral for evaluating how composite laminates resist notch-tip damage and crack growth under opening mode loading. It applies to composites of varying fiber orientations, thicknesses, and matrix types, using results from tension testing of monotonically loaded, notched specimens at room temperature.
Fracture toughness measurements are essential for research and development, structural design, and quality control in industries that rely on the structural integrity and durability of composite materials, such as aerospace, automotive, wind energy, and civil engineering.
Key Topics
-
Translaminar Fracture Toughness (KTL):
- Provides a quantitative measure of a composite laminate's resistance to crack growth and propagation from notches under tensile stress.
- KTL validity relies on keeping the damage zone at the notch tip small compared to the notch length and in-plane specimen dimensions.
-
Applicability:
- Suited to a broad range of composite materials including carbon fiber-epoxy, glass fiber-epoxy, glass fiber-polyester pultrusions, and carbon fiber-bismaleimide laminates.
- Not limited by thickness, polymer matrix, or fiber type, provided the specimen meets dimensional and test requirements.
-
Test Configurations and Environments:
- Involves eccentrically loaded, single-edge-notch tension (ESE(T)) specimens.
- Applicable to room temperature laboratory environments; other conditions may apply if requirements are met.
-
Damage Characterization:
- If extensive distributed damage occurs, the test still provides valid structural response data, such as force-displacement behavior and damage events, useful for validating composite damage models.
-
Specimen Requirements:
- Multidirectional fiber orientation, accurate specimen geometry, and precise notch preparation are critical for reliable results.
- Requires careful documentation of material properties, fabrication methods, and test conditions.
-
Reporting:
- Comprehensive reporting of specimen preparation, testing procedure, material identification, notch dimensions, environmental data, and statistical measures of fracture toughness and damage events.
Applications
-
Research & Development:
- Enables quantification of how fiber and matrix variables or stacking sequences influence the fracture resistance of polymer matrix composites.
- Supports the validation of progressive damage models for new composite formulations and structures.
-
Structural Design:
- Provides critical data to assess the resistance of composite laminates to edge flaws and notches, supporting damage tolerance criteria in structural components.
- Facilitates safer, more efficient design of lightweight structures used in transportation, energy, and infrastructure.
-
Quality Control & Specification:
- Ensures manufacturing consistency by establishing acceptance criteria for composite panels and components.
- Helps identify material or fabrication process variations that affect structural performance.
-
Validation of Numerical and Analytical Models:
- Force-displacement and discrete damage data can be used to validate finite element or damage mechanics models, improving predictive maintenance and design optimization.
Related Standards
- ASTM D3039/D3039M - Test Method for Tensile Properties of Polymer Matrix Composite Materials
- ASTM D3171 - Test Methods for Constituent Content of Composite Materials
- ASTM D5528/D5528M - Test Method for Mode I Interlaminar Fracture Toughness of Unidirectional Fiber-Reinforced Composites
- ASTM D5687/D5687M - Guide for Preparation of Flat Composite Panels
- ASTM E399 - Test Method for Linear-Elastic Plane-Strain Fracture Toughness of Metallic Materials
- ASTM D792 - Density and Specific Gravity (Relative Density) of Plastics by Displacement
ASTM E1922/E1922M-22 is a key resource for anyone involved in the testing, design, or certification of polymer matrix composite materials, ensuring reliable and comparable assessment of translaminar fracture properties across the global composites industry. For implementation and full technical guidance, always refer to the latest official ASTM edition.
Технические детали
- Технический комитет
- D30 - Composite Materials
- SKU
- ASTM E1922/E1922M-22
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