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ASTM D7615/D7615M-19

Standard Practice for Open-Hole Fatigue Response of Polymer Matrix Composite Laminates

Pages: 8
Publication date: 2019-04-01
Price: 48 vnd

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1.1 This practice provides instructions for modifying static open-hole tensile and compressive strength test methods to determine the fatigue behavior of composite materials subjected to cyclic tensile or compressive forces, or both. The composite material forms are limited to continuous-fiber reinforced polymer matrix composites in which the laminate is both symmetric and balanced with respect to the test direction. The range of acceptable test laminates and thicknesses are described in 8.2. 1.2 This practice supplements Test Methods D5766/D5766M and D6484/D6484M with provisions for testing specimens under cyclic loading. Several important test specimen parameters, for example fatigue force (stress) ratio, are not mandated by this practice; however, repeatable results require that these parameters be specified and reported. 1.3 This practice is limited to test specimens subjected to constant amplitude uniaxial loading, where the machine is controlled so that the test specimen is subjected to repetitive constant amplitude force (stress) cycles. Either engineering stress or applied force may be used as a constant amplitude fatigue variable. The repetitive loadings may be tensile, compressive, or reversed, depending upon the test specimen and procedure utilized. 1.4 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. 1.4.1 Within the text the inch-pound units are shown in brackets. 1.5 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. 1.6 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.
Document identifier
ASTM D7615/D7615M-19
Title
Standard Practice for Open-Hole Fatigue Response of Polymer Matrix Composite Laminates
ASTM Category
Volume 15.03 - Space Simulation; Aerospace and Aircraft; High Modulus Fibers
Publication date
2019-04-01
Status
Effective
International Relationship
Cross references
Latest version
ASTM D7615/D7615M-19
Standard Practice for Open-Hole Fatigue Response of Polymer Matrix Composite Laminates
Document identifier ASTM D7615/D7615M-19
Publication date 2019-04-01
Classification 83.120. Reinforced plastics
Status Effective
*
History of version
ASTM D7615/D7615M-19 * ASTM D7615/D7615M-11(2018) * ASTM D7615/D7615M-11
Keywords
Pages
8
Price 48 vnd