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ASTM E 290 : 2014 : REDLINE

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

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Standard Test Methods for Bend Testing of Material for Ductility

Available format(s)

PDF

Superseded date

28-09-2022

Language(s)

English

Published date

12-09-2014

€67.30
Excluding VAT

CONTAINED IN VOL. 03.01, 2015 Describes bend testing for ductility of materials.

Committee
E 28
DocumentType
Redline
Pages
10
PublisherName
American Society for Testing and Materials
Status
Superseded
SupersededBy

1.1These test methods cover bend testing for ductility of materials. Included in the procedures are four conditions of constraint on the bent portion of the specimen; a guided-bend test using a mandrel or plunger of defined dimensions to force the mid-length of the specimen between two supports separated by a defined space; a semi-guided bend test in which the specimen is bent, while in contact with a mandrel, through a specified angle or to a specified inside radius (r) of curvature, measured while under the bending force; a free-bend test in which the ends of the specimen are brought toward each other, but in which no transverse force is applied to the bend itself and there is no contact of the concave inside surface of the bend with other material; a bend and flatten test, in which a transverse force is applied to the bend such that the legs make contact with each other over the length of the specimen.

1.2After bending, the convex surface of the bend is examined for evidence of a crack or surface irregularities. If the specimen fractures, the material has failed the test. When complete fracture does not occur, the criterion for failure is the number and size of cracks or surface irregularities visible to the unaided eye occurring on the convex surface of the specimen after bending, as specified by the product standard. Any cracks within one thickness of the edge of the specimen are not considered a bend test failure. Cracks occurring in the corners of the bent portion shall not be considered significant unless they exceed the size specified for corner cracks in the product standard.

1.3The values stated in SI units are to be regarded as standard. Inch-pound values given in parentheses were used in establishing test parameters and are for information only.

1.4This 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.

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SAE AMS 5544 : 2014 NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 57NI - 19.5CR - 13.5CO - 4.2MO - 3.0TI - 1.4AL - 0.05ZR - 0.006B, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, ANNEALED
SAE AMS 5596 : 2017 NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, FOIL AND PLATE, 52.5NI - 19CR - 3.0MO - 5.1CB (NB) - 0.90TI - 0.50AL - 18FE, CONSUMABLE ELECTRODE REMELTED OR VACUUM INDUCTION MELTED, 1775 DEGREES F (968 DEGREES C) SOLUTION HEAT TREATED
SAE AMS 5597 : 2016 NICKEL ALLOY, CORROSION AND HEAT RESISTANT, SHEET, STRIP, AND PLATE, 52.5NI - 19CR - 3.0MO - 5.1CB (NB) - 0.90TI - 0.50AL - 18FE, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, 1950 DEGREES F (1066 DEGREES C) SOLUTION HEAT TREATED
ASTM B 236M : 2007 Standard Specification for Aluminum Bars for Electrical Purposes (Bus Bars) [Metric]
16/30338812 DC : 0 BS EN ISO 8401 - METALLIC COATINGS - REVIEW OF METHODS OF MEASUREMENT OF DUCTILITY
SAE AMS 5547 : 2012 STEEL, CORROSION AND HEAT-RESISTANT, SHEET AND STRIP, 15.5CR - 4.5NI - 2.9MO - 0.10N, SOLUTION HEAT TREATED
ASTM A 721/A721M : 2002 : R2011 Standard Test Method for Ductility of Oriented Electrical Steel
SAE AMS 6951 : 2017 TITANIUM ALLOY, SHEET 5AL - 4V - 0.75MO - 0.5FE ANNEALED
QQ-C-530 Revision C:1971 COPPER BERYLLIUM ALLOY BAR, ROD, AND WIRE (COPPER ALLOY NUMBERS 172 AND 173)
SAE AMS 6395 : 2015 STEEL SHEET, STRIP, AND PLATE, 0.95CR - 0.20MO (0.38 - 0.43C) (SAE 4140)
MIL-N-62418 Base Document:1992 NICKEL BASE ALLOY, SHEET & PLATE CORROSION & HEAT RESISTANT, SOLUTION HEAT TREATED (HAYNES 230) (METRIC)
SAE AMS 4908 : 1988 TITANIUM ALLOY, SHEET AND STRIP 8MN ANNEALED, 110 KSI (758 MPA) YIELD STRENGTH
ASTM B 169/B169M : 2015 : REDLINE Standard Specification for Aluminum Bronze Sheet, Strip, and Rolled Bar
MIL-B-46066 Revision B:1983 BANDS, ROTATING, COPPER ALLOY, CENTRIFUGAL CAST (FOR CRITICAL APPLICATIONS)
ASTM B 249M : 1994 SPECIFICATION FOR GENERAL REQUIREMENTS FOR WROUGHT COPPER AND COPPER ALLOY ROD, BAR, SHAPES AND FORGINGS (METRIC)
ASTM B 740 : 2009 : R2015 Standard Specification for Copper-Nickel-Tin Spinodal Alloy Strip
SAE AMS 5912 : 2014 STEEL, CORROSION-RESISTANT, SHEET AND STRIP, 19CR - 9.2NI (SAE 30304), COLD ROLLED, 3/4 HARD, 175 KSI (1207 MPA) TENSILE STRENGTH
SAE AMS 5607 E: 2012 NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 73NI - 7.0CR - 16.5MO, SOLUTION HEAT TREATED
SAE AMS 5517 : 2010 STEEL, CORROSION RESISTANT, SHEET AND STRIP, 18CR - 8NI (301) COLD ROLLED, 125 KSI (862 MPA) TENSILE STRENGTH
SAE AMS 4915 : 2017 TITANIUM ALLOY SHEET, STRIP, AND PLATE 8AL - 1V - 1MO SINGLE ANNEALED
SAE AMS4897D : 2016 TITANIUM ALLOY, SHEET AND STRIP, 15MO - 3.0AL - 2.8CB - 0.20SI
SAE AMS 5608 : 2016 COBALT ALLOY, CORROSION AND HEAT RESISTANT, SHEET, STRIP, AND PLATE, 40CO - 22CR - 22NI - 14.5W - 0.07LA, SOLUTION HEAT TREATED
SAE AMS 4989 : 2014 TITANIUM ALLOY SHEET, STRIP, AND PLATE, 3AL - 2.5V, ANNEALED
SAE AMS QQ A 250 B : 2012 ALUMINUM AND ALUMINUM ALLOY, PLATE AND SHEET GENERAL SPECIFICATION FOR
SAE AMS 6354 : 2016 STEEL, SHEET, STRIP, AND PLATE, 0.75SI - 0.62CR - 0.20MO - 0.10ZR (0.10 - 0.17C)
SAE AMS C 81769 : 2015 CHEMICAL MILLING OF METALS, SPECIFICATION FOR
SAE AMS 5901B:2008 STEEL, CORROSION-RESISTANT, SHEET, STRIP, AND PLATE, 18CR - 8NI (SAE 30301), SOLUTION HEAT TREATED
SAE AMS 4918 : 2014 TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 6AL - 6V - 2SN, ANNEALED
SAE AMS 5869 : 2013 NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE 62NI - 21.5CR - 9.0MO - 3.7CB SOLUTION HEAT TREATED
SAE AMS 5904 : 2012 STEEL, CORROSION-RESISTANT, SHEET AND STRIP, 18CR - 9.0NI (SAE 30302), COLD ROLLED, 1/2 HARD, 150 KSI (1034 MPA) TENSILE STRENGTH
SAE AMS 5540 : 2017 NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 74NI - 15.5CR - 8.0FE, ANNEALED
SAE AMS QQ A 225 : 2018 ALUMINUM AND ALUMINUM ALLOY, BAR, ROD, WIRE OR SPECIAL SHAPES; ROLLED, DRAWN OR COLD FINISHED; GENERAL SPECIFICATION FOR
SAE AMS 6437 : 2015 STEEL, SHEET, STRIP, AND PLATE, 5.0CR - 1.3MO - 0.50V (0.38 - 0.43C) (H-11)
SAE AMS 5905 : 2012 STEEL, CORROSION-RESISTANT, SHEET AND STRIP, 18CR - 9.0NI (SAE 30302), COLD ROLLED, 3/4 HARD, 175 KSI (1207 MPA) TENSILE STRENGTH
SAE AMS 5550F :1988(S2017) ALLOY SHEET, STRIP, AND PLATE, CORROSION AND HEAT RESISTANT, 80NI - 15.5CR - 0.62TI - 3.25AL, ANNEALED
SAE AMS 7847D : 2015 TANTALUM ALLOY SHEET, STRIP, AND PLATE, 90TA - 10W
SAE AMS 5542 : 2012 NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 72NI - 15.5CR - 0.95CB(NB) - 2.5TI - 0.70AL - 7.0FE, ANNEALED
SAE AMS 5506 : 2018 STEEL, CORROSION AND HEAT RESISTANT, SHEET, STRIP, AND PLATE, 13CR (0.30 - 0.40C) (420), ANNEALED
SAE AMS 2441 : 2000 SELECTIVE (BRUSH) NICKEL PLATING LOW-STRESSED, LOW HARDNESS DEPOSIT
ASTM F 67 : 2013 Standard Specification for Unalloyed Titanium, for Surgical Implant Applications (UNS R50250, UNS R50400, UNS R50550, UNS R50700)
ASTM F 3122 : 2014 Standard Guide for Evaluating Mechanical Properties of Metal Materials Made via Additive Manufacturing Processes
ASTM F 3160 : 2016 Standard Guide for Metallurgical Characterization of Absorbable Metallic Materials for Medical Implants
SAE AMS 2399 : 2011 ELECTROLESS NICKEL-BORON PLATING
DIN EN ISO 8401:2016-08 (Draft) METALLIC COATINGS - REVIEW OF METHODS OF MEASUREMENT OF DUCTILITY (ISO 8401:2017)
ISO 8401:2017 Metallic coatings — Review of methods of measurement of ductility
EN ISO 8401:2017 Metallic coatings - Review of methods of measurement of ductility (ISO 8401:2017)
SAE AMS 6356 : 2015 STEEL, SHEET, STRIP, AND PLATE, 0.95CR - 0.20MO - (0.30 - 0.35C) (4132)
SAE AMS 4720 : 2016 WIRE, PHOSPHOR BRONZE, 94CU - 5.0SN - 0.19P, COLD DRAWN, SPRING TEMPER (H08)
ASTM B 551/B551M : 2012 Standard Specification for Zirconium and Zirconium Alloy Strip, Sheet, and Plate
ASTM B 209M : 2014 : REDLINE Standard Specification for Aluminum and Aluminum-Alloy Sheet and Plate (Metric)
QQ C 00465 : B COPPER ALUMINUM ALLOYS (ALUMINUM BRONZE) (COPPER ALLOY NUMBERS 606, 614, 630, 632M, AND 642), ROD, FLAT PRODUCTS WITH FINISHED EDGES (FLAT WIRE, STRIP, AND BAR), SHAPES, AND FORGINGS)
MIL-DTL-24625 Revision A:2009 ANODES, IMPRESSED CURRENT CATHODIC PROTECTION - PLATINIZED TYPE
SAE AMS 5519 : 2014 STEEL, CORROSION RESISTANT, SHEET AND STRIP, 18CR - 8NI (SAE 30301) COLD ROLLED, 185 KSI (1276 MPA) TENSILE STRENGTH
ASTM A 706/A706M : 2016 : REDLINE Standard Specification for Deformed and Plain Low-Alloy Steel Bars for Concrete Reinforcement
SAE AMS 5863E : 2009(R2015) STEEL, CORROSION RESISTANT, SHEET, STRIP, AND PLATE, 15CR - 6.5NI - 0.75MO - 0.60CB - 1.5CU, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE
SAE AMS 7817 : 1978 MOLYBDENUM ALLOY SHEET, STRIP, AND PLATE, 0.48TI - 0.090ZR - 0.02C, ARC CAST, STRESS RELIEVED
MIL-DTL-18001 Revision L:2013 ANODES, SACRIFICIAL ZINC ALLOY
MIL-DTL-24779 Revision D:2015 ANODES, SACRIFICIAL, ALUMINUM ALLOY
MIL-DTL-46177 Revision C:1998 Armor, Steel Plate and Sheet, Wrought, Homogeneous (1/8 to Less Than 1/4 Inch Thick)
SAE AMS 5871 : 2015 ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP AND PLATE, 21CR - 32.5NI - 0.38TI - 0.38AL - 45FE, SOLUTION HEAT TREATED
SAE AMS 5595 : 2014 STEEL, CORROSION RESISTANT, SHEET, STRIP, AND PLATE, 9.0MN - 20CR - 6.5NI - 0.28N, SOLUTION HEAT TREATED
MIL-F-50950 Revision C:1993 FUZE, GRENADE, GP: M223
QQ C 586 : C COPPER NICKEL ZINC ALLOY, ROD, SHAPES, FLAT PRODUCTS WITH FINISHED EDGES (FLAT WIRE, STRIP, AND BAR)
SAE AMS 5537 : 2017 COBALT ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, FOIL, AND PLATE, 52CO - 20CR - 10NI - 15W, SOLUTION HEAT TREATED
ASTM A 880 : 1995 Standard Practice for Criteria for Use in Evaluation of Testing Laboratories and Organizations for Examination and Inspection of Steel, Stainless Steel, and Related Alloys (Withdrawn 2004)
SAE AMS 5606 : 2013 ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE 41.5NI - 16CR - 37FE - 2.9CB (NB) - 1.8TI CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED 1750 DEGREES F (954 DEGREES C) SOLUTION HEAT TREATED
MIL-C-10147 Revision D:1984 CABINET, PHOTOGRAPHIC STORAGE, FILM BM-11( )
SAE AMS 5599 : 2016 NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 62NI - 21.5CR - 9.0MO - 3.7 CB (NB), ANNEALED
SAE AMS 6357 : 2015 STEEL SHEET, STRIP, AND PLATE, 0.50CR - 0.55NI - 0.25MO (0.33 - 0.38C) (8735)
SAE AMS 5503 : 2015 STEEL, CORROSION-RESISTANT, SHEET, STRIP, AND PLATE, 17CR (SAE 51430) ANNEALED
SAE AMS7301J:2003(S2017) Steel, Highly-Stressed Springs 0.95Cr - 0.20V (0.48 - 0.53C) (SAE 6150) Case Hardened(STABILIZED Aug 2017)
SAE AMS 5605 : 2013 NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 41.5NI - 16CR - 37FE - 2.9CB(NB) - 1.8TI, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, 1800 DEGREES F (982 DEGREES C) SOLUTION HEAT TREATED
SAE AMS 5906C : 2018 STEEL, CORROSION-RESISTANT, SHEET AND STRIP, 18CR - 9.0NI (SAE 30302), COLD ROLLED, FULL HARD, 185 KSI (1276 MPA) TENSILE STRENGTH
SAE AMS 7850 : 2013 COLUMBIUM (NIOBIUM) SHEET, STRIP, AND FOIL
SAE AMS 4902 : 2013 TITANIUM SHEET, STRIP, AND PLATE, COMMERCIALLY-PURE, ANNEALED 40.0 KSI (276 MPA) YIELD STRENGTH
SAE AMS 2368 : 2017 SAMPLING AND TESTING OF WROUGHT TITANIUM RAW MATERIAL EXCEPT FORGINGS AND FORGING STOCK
SAE AMS 4279 : 2011 ALUMINUM ALLOY, ALCLAD SHEET, 4.4CU - 1.5MG - 0.60MN (2024 -T4 FLAT SHEET), SOLUTION HEAT TREATED, HIGH FORMABILITY
SAE AMS 4899 : 2016 TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 4.5AI - 3V - 2FE - 2MO, ANNEALED
SAE AMS 6454 : 2011 STEEL, SHEET, STRIP, AND PLATE, 1.8NI - 0.80CR - 0.25MO (0.38 - 0.43C) (SAE 4340) VACUUM CONSUMABLE ELECTRODE REMELTED
SAE AMS 5950 : 2014 NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET AND STRIP 52.5NI - 19CR - 3.0MO - 5.0CB - 0.90TI - 0.50AL - 18FE VACUUM INDUCTION AND CONSUMABLE ELECTRODE MELTED SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE
ASTM A 720/A720M : 2002 : R2011 Standard Test Method for Ductility of Nonoriented Electrical Steel
ASTM A 721/A721M : 2002 : R2007 Standard Test Method for Ductility of Oriented Electrical Steel
SAE AMS 6345 : 2015 STEEL, SHEET, STRIP, AND PLATE, 0.95CR - 0.20MO (0.28 - 0.33C) (SAE 4130), NORMALIZED OR OTHERWISE HEAT TREATED
SAE AMS 5512 : 2012 STEEL, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 18CR - 10.5NI - 0.80CB (SAE 30347), SOLUTION HEAT TREATED
ASTM F 2066 : 2018 : REDLINE Standard Specification for Wrought Titanium-15 Molybdenum Alloy for Surgical Implant Applications (UNS R58150)
ASTM A 1058 : 2014 : REDLINE Standard Test Methods for Mechanical Testing of Steel Products—Metric
ASTM B 211M : 2012 Standard Specification for Aluminum and Aluminum-Alloy Rolled or Cold-Finished Bar, Rod, and Wire (Metric)
ASTM F 67 : 2013 : R2017 Standard Specification for Unalloyed Titanium, for Surgical Implant Applications (UNS R50250, UNS R50400, UNS R50550, UNS R50700)
ASTM A 721/A721M : 2002 : R2016 Standard Test Method for Ductility of Oriented Electrical Steel
ASTM A 721/A721M : 2002 Standard Test Method for Ductility of Oriented Electrical Steel
BS EN ISO 8401:2017 Metallic coatings. Review of methods of measurement of ductility
ASME B18.29.1 : 2010 : R2017 Helical Coil Screw Thread Inserts--Free Running and Screw Locking (Inch Series) (B18.29.1 - 2010)
ASME B18.29.1 : 2010 HELICAL COIL SCREW THREAD INSERTS - FREE RUNNING AND SCREW LOCKING (INCH SERIES)
ASME B18.29.2M:2005 HELICAL COIL SCREW THREAD INSERTS: FREE RUNNING AND SCREW LOCKING (METRIC SERIES)
ASME B18.29.2M : 2005 : R2017 HELICAL COIL SCREW THREAD INSERTS: FREE RUNNING AND SCREW LOCKING (METRIC SERIES)

ASTM E 190 : 2014 : REDLINE Standard Test Method for Guided Bend Test for Ductility of Welds
ASTM E 8/E8M : 2016-09 TEST METHODS FOR TENSION TESTING OF METALLIC MATERIALS

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