ASTM B909-00(2006) - 1.9.2006
 
1. Scope

1.1 This guide covers supplementary guidelines for plane-strain fracture toughness testing of aluminum products for which complete stress relief is not practicable. Guidelines for recognizing when residual stresses may be significantly biasing test results are presented, as well as methods for minimizing the effects of residual stress during testing. This guide also provides guidelines for correction and interpretation of data produced during the testing of these products. Test Method E 399 is the standard test method to be used for plane-strain fracture toughness testing of aluminum alloys.

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 and health practices and determine the applicability of regulatory limitations prior to use.

 
2. Referenced Documents

E561-23

Standard Test Method for KR Curve Determination

E1823-26a

Standard Terminology Relating to Fatigue and Fracture Testing (Includes all amendments and changes 8/27/2026).

E399-24

Standard Test Method for Linear-Elastic Plane-Strain Fracture Toughness of Metallic Materials

ISO 12737

Metallic Materials-Determination of Plane Strain Fracture Toughness Available from International Organization for Standardization (ISO), 1 rue de Varemb, Case postale 56, CH-1211, Geneva 20, Switzerland, http://www.iso.ch.

ANSI H35.1

Alloy and Temper Designations for Aluminum Available from American National Standards Institute (ANSI), 25 W. 43rd St., 4th Floor, New York, NY 10036, http://www.ansi.org.