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About This Item

 

Full Description

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 values stated in either SI units or inch-pound units are to be regarded separately as standard. Within the text the inch-pound units are shown in brackets. The values stated in each system are not exact equivalents; therefore, each system must be used independently of the other. Combining values from the two systems may result in nonconformance with the test method.

1.3 This standard does not purport to address all of the safety problems, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.

 

Document History

  1. ASTM D5448/D5448M-22


    Standard Test Method for Inplane Shear Properties of Hoop Wound Polymer Matrix Composite Cylinders

    • Most Recent
  2. ASTM D5448/D5448M-16


    Standard Test Method for Inplane Shear Properties of Hoop Wound Polymer Matrix Composite Cylinders

    • Historical Version
  3. ASTM D5448/D5448M-11

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    Standard Test Method for Inplane Shear Properties of Hoop Wound Polymer Matrix Composite Cylinders

    • Historical Version
  4. ASTM D5448/D5448M-93(2006)


    Standard Test Method for Inplane Shear Properties of Hoop Wound Polymer Matrix Composite Cylinders

    • Historical Version
  5. ASTM D5448/D5448M-93(2000)


    Standard Test Method for Inplane Shear Properties of Hoop Wound Polymer Matrix Composite Cylinders

    • Historical Version
  6. ASTM D5448/D5448M-93


    Standard Test Method for Inplane Shear Properties of Hoop Wound Polymer Matrix Composite Cylinders

    • Historical Version