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ASTM E 602 : 2003

Withdrawn
Withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

Standard Test Method for Sharp-Notch Tension Testing with Cylindrical Specimens (Withdrawn 2010)
Available format(s)

Hardcopy , PDF

Withdrawn date

10-31-2010

Language(s)

English

Published date

05-10-2003

CONTAINED IN VOL. 03.01, 2009 Includes determination of a comparative measure of the resistance of thick-section materials to fracture under plane-strain conditions originating from a very sharp stress-concentrator or crack.

1.1 This test method covers the determination of a comparative measure of the resistance of thick-section materials to fracture under plane-strain conditions originating from a very sharp stress-concentrator or crack (Note 1). The quantity determined is the sharp-notch strength of a specimen of particular dimensions, and this value depends upon these dimensions as well as the characteristics of the material. The sharp-notch strength-to-yield strength ratio is also determined.

Note 1—Direct measurements of the plane-strain fracture toughness may be made in accordance with Test Method E 399. Comparative measures of resistance to fracture for sheet and thin plate may be obtained in accordance with Test Method E 338.

1.2 This test method is restricted to sharp machine-notched specimens (notch tip radii less than or equal to 0.018 mm (0.0007 in.)), and applies only to those materials (for example, aluminum and magnesium alloys) in which such sharp notches can be reproducibly machined.

1.3 This test method is restricted to cylindrical specimens of two diameters as shown in . The 27.0-mm (1 1/16- in.) diameter specimen extends the range of application of this test method to higher toughness levels than could be accommodated by the 12.7-mm (0.5-in.) diameter specimen.

1.4 This test method is restricted to materials equal to or greater than 12.7 mm (0.5 in.) in thickness. Since the notch strength depends on the specimen diameter and, within certain limits, on the length, comparison of various material conditions must be based on tests of specimens having the same nominal diameter and a test section length sufficient to prevent significant interaction between the stress field of the specimen heads and that of the sharp notch (see Fig. 1).

1.5 The sharp-notch strength may depend strongly upon temperature within a certain range depending upon the characteristics of the material. This test method is suitable for tests at any appropriate temperature. However, comparisons of various material conditions must be based on tests conducted at the same temperature.

1.6 The values stated in SI (metric) units are to be regarded as the standard.

Note 2—Further information on background and need for this type of test is given in the Fourth Report of ASTM Committee E-24 (1) on Fracture Testing, as well as other committee documents (2, 3, 4).

1.7 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.

Committee
E 08
DocumentType
Test Method
Pages
7
PublisherName
American Society for Testing and Materials
Status
Withdrawn
Supersedes

SAE AMS 4306 : 2018 ALUMINUM ALLOY, PLATE, 6.4ZN - 2.4MG - 2.2CU - 0.12ZR (7150-T6151), SOLUTION HEAT TREATED, STRESS RELIEVED, AND AGED
ASTM E 616 : 1989 Terminology Relating to Fracture Testing (Withdrawn 1996)
ASTM E 338 : 2003 Standard Test Method of Sharp-Notch Tension Testing of High-Strength Sheet Materials (Withdrawn 2010)
ASTM G 129 : 2000 : R2006 Standard Practice for Slow Strain Rate Testing to Evaluate the Susceptibility of Metallic Materials to Environmentally Assisted Cracking
ASTM B 865 : 2004 : R2010 Standard Specification for Precipitation Hardening Nickel-Copper-Aluminum Alloy (UNS N05500) Bar, Rod, Wire, Forgings, and Forging Stock
PREN 6071 : 200P1 AEROSPACE SERIES - ALUMINIUM AND ALUMINIUM ALLOY WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PLATE
SAE AMS 4202 : 2005 ALUMINUM ALLOY, PLATE - 5.7ZN - 2.2MG - 1.6CU - 0.22CR (7475-T7351), SOLUTION HEAT TREATED, STRESS RELIEVED BY STRETCHING, AND PRECIPITATION HEAT TREATED
SAE AMS 4204 : 2013 ALUMINUM ALLOY, PLATE, 6.2ZN - 1.8CU - 2.4MG - 0.13ZR (7010-T7651), SOLUTION HEAT TREATED, STRESS RELIEVED, AND PRECIPITATION HEAT TREATED
ASTM B 865 : 2004 Standard Specification for Precipitation Hardening Nickel-Copper-Aluminum Alloy (UNS N05500) Bar, Rod, Wire, Forgings, and Forging Stock
ASTM G 129 : 2000 : R2013 Standard Practice for Slow Strain Rate Testing to Evaluate the Susceptibility of Metallic Materials to Environmentally Assisted Cracking
ASME PV CODE 8 DIV 3 : 2017 BPVC Section VIII-BOILER AND PRESSURE VESSEL CODE - RULES FOR CONSTRUCTION OF PRESSURE VESSELS - ALTERNATIVE RULES FOR CONSTRUCTION OF HIGH PRESSURE VESSELS
ASTM G 129 : 2000 Standard Practice for Slow Strain Rate Testing to Evaluate the Susceptibility of Metallic Materials to Environmentally Assisted Cracking
DIN 29546:1990-10 Aerospace; wrought aluminium alloys sheet, plate and strip; technical specification; inactive for new design
PREN 2002-23 : 200P1 AEROSPACE SERIES - TEST METHODS FOR METALLIC MATERIALS - PART 23 - SHARP-NOTCH TENSION TESTING
96/716568 DC : 0 PREN 4400-2 - AEROSPACE SERIES - ALUMINIUM AND ALUMINIUM ALLOY WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 2: PLATE
ASTM B 865 : 2004 : R2015 Standard Specification for Precipitation Hardening Nickel-Copper-Aluminum Alloy<brk/> (UNS N05500) Bar, Rod, Wire, Forgings, and Forging Stock

ASTM B 557 : 2015 : REDLINE Standard Test Methods for Tension Testing Wrought and Cast Aluminum- and Magnesium-Alloy Products
ASTM E 338 : 2003 Standard Test Method of Sharp-Notch Tension Testing of High-Strength Sheet Materials (Withdrawn 2010)
ASTM E 8 : 2004 Standard Test Methods for Tension Testing of Metallic Materials

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