ASTM D5448/D5448M-22
Standard Test Method for Inplane Shear Properties of Hoop Wound Polymer Matrix Composite Cylinders
Standard Test Method for Inplane Shear Properties of Hoop Wound Polymer Matrix Composite Cylinders
- Статус документа:
- Действующий
- Формат:
- Электронный (PDF)
- Количество страниц:
- 13
- Дата публикации:
- 1 мая 2022 г.
- Издание:
- D5448/D5448M
- ICS:
- 83.120
SIGNIFICANCE AND USE 5.1 This test method is designed to produce inplane shear property data for material specifications, research and development, quality assurance, and structural design and analysis. Factors that influence the inplane shear response and should therefore be reported are material, method of material preparation, specimen preparation, specimen conditioning, environment of testing, specimen alignment and gripping, speed of testing, void content, and fiber volume fraction. Properties, in the test direction, that may be obtained from this test method are as follows: 5.1.1 Inplane Shear Strength, τ12u, 5.1.2 Inplane Shear Strain at Failure, γ12u , and 5.1.3 Inplane Shear Modulus, G12. SCOPE 1.1 This test method determines the inplane shear properties of wound polymer matrix composites reinforced by high-modulus continuous fibers. It describes testing of hoop wound (90°) cylinders in torsion for determination of inplane shear properties. 1.2 The technical content of this test method has been stable since 1993 without significant objection from its stakeholders. As there is limited technical support for the maintenance of this test method, changes since that date have been limited to items required to retain consistency with other ASTM D30 Committee standards, including editorial changes and incorporation of updated guidance on specimen preconditioning and environmental testing. The test method, therefore, should not be considered to include any significant changes in approach and practice since 1993. Future maintenance of the test method will only be in response to specific requests and performed only as technical support allows. 1.3 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. 1.3.1 Within the text, the inch-pound units are shown in brackets. 1.4 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use. 1.5 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.
Abstract
Overview
ASTM D5448/D5448M-22 is an internationally recognized standard test method developed by ASTM International for determining the inplane shear properties of hoop wound polymer matrix composite cylinders. This standard is indispensable for professionals involved in material specifications, research and development, quality assurance, and structural analysis of composite materials. It focuses on high-modulus continuous fiber-reinforced polymer matrix composites, examining the torsional response of hoop wound (90°) cylindrical specimens.
This test method provides valuable data on the inplane shear strength, inplane shear strain at failure, and inplane shear modulus of composite materials, supporting optimization and safety in engineering applications.
Key Topics
- Shear Properties Measurement: The method estimates:
- Inplane shear strength (τ12u)
- Inplane shear strain at failure (γ12u)
- Inplane shear modulus (G12)
- Applicability: Specifically designed for hoop wound composite cylinders, typically fabricated using high-modulus, continuous fiber reinforcement.
- Test Procedure Highlights:
- Cylindrical specimens are loaded in torsion using specialized fixtures to produce and measure inplane shear properties.
- Measurements utilize resistance strain gauges, with correction for transverse sensitivity and temperature effects.
- Specimen and fixture preparation, system alignment, and environmental conditioning are essential to achieving accurate results.
- Reporting Factors: Key factors affecting test results include material type, method of manufacture, specimen preparation, test environment, conditioning, alignment, gripping method, testing speed, void content, and fiber volume fraction.
- Data Analysis: Results are calculated per specimen and require statistical treatment (mean, standard deviation, coefficient of variation) for series of tests.
Applications
ASTM D5448/D5448M-22 is widely used in industries where advanced composite materials are critical, including:
- Aerospace Engineering: Ensures reliable material performance in load-bearing components of aircraft and spacecraft, especially in pressurized cylinders and tanks.
- Automotive and Transport: Supports the structural design and quality control of composite drive shafts and pressure vessels.
- Civil Infrastructure: Utilized for composite piping and pressure containment systems in construction and utilities.
- Material R&D: Facilitates comparison of new composite formulations, supporting material innovation by delivering standardized strength and modulus data.
- Quality Control: Assists manufacturers and suppliers in meeting material specifications and maintaining consistent production quality.
Related Standards
ASTM D5448/D5448M-22 references several key ASTM standards for composite material testing and data analysis:
- ASTM D792: Test Methods for Density and Specific Gravity of Plastics
- ASTM D883: Terminology Relating to Plastics
- ASTM D2584: Test Method for Ignition Loss of Cured Reinforced Resins
- ASTM D2734: Test Methods for Void Content of Reinforced Plastics
- ASTM D3171: Test Methods for Constituent Content of Composite Materials
- ASTM D3878: Terminology for Composite Materials
- ASTM D5229/D5229M: Moisture Absorption and Conditioning of Composite Materials
- ASTM D5449/D5449M, D5450/D5450M: Related test methods for transverse properties of hoop wound cylinders
- ASTM E6, E111: Mechanical testing terminology and modulus of elasticity determination
For effective use of ASTM D5448/D5448M-22, it is important to apply consistent terminology and supporting test methods within the broader context of ASTM composite testing standards.
Keywords: ASTM D5448/D5448M-22, inplane shear properties, hoop wound polymer matrix composite cylinders, composite material testing, shear strength, shear modulus, quality assurance, structural analysis, fiber-reinforced composites, material standards, ASTM composite test methods.
Технические детали
- Технический комитет
- D30 - Composite Materials
- SKU
- ASTM D5448/D5448M-22
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