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unnotched specimen
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Image
Published: 01 January 1987
Fig. 1015 Surface of a tension-overload fracture in an unnotched specimen of aluminum alloy 7075-T6 having a tensile strength of 520 MPa (75 ksi), with 22% reduction of area. Surface is coarsely fibrous; shear lip has formed two opposing lobes. See also Fig. 1016 and 1017 . 9×
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Image
Published: 01 January 1987
Fig. 1162 Tensile-overload fracture surface of an unnotched specimen of titanium alloy Ti-6Al-4V heat treated to tensile strength of 1158.8 MPa (168.5 ksi) and 47% reduction of area. A classic example of cup-and-cone fracture having a flat, fibrous central zone. See also Fig. 1163 . 9×
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Image
Published: 01 January 1987
Fig. 391 Surface of a fracture in an unnotched specimen of AISI 4340 steel that was broken in tension overload, displaying elongated and quite flat shear dimples. Note that some crude steps have formed, which suggests that there may have been some degree of pulsation in the applied stress
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Image
Published: 01 January 1987
Fig. 530 Tensile-overload fracture in an unnotched specimen of AISI 8740 steel; tensile strength, 1351 MPa (196 ksi). A cup-and-cone fracture with a fibrous zone containing radial features between the central fibrous region and the shear lip. See also Fig. 531 and 532 . 9×
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Image
Published: 01 January 1987
Fig. 774 Tension-overload fracture in an unnotched specimen of AISI H11 tool steel heat treated to a tensile strength of 2041 MPa (296 ksi) and 48% reduction of area. Note radial features between fibrous origin (just right of center) and shear lip. See also Fig. 775 and 776 for higher
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Book Chapter
Book: Fatigue and Fracture
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002415
EISBN: 978-1-62708-193-1
... properties and damage tolerance of fiber-metal laminates such as ARALL and GLARE laminates. The article concludes with a discussion on the effects of fatigue on notched and unnotched specimens. ARALL laminates composite laminates damage tolerance delamination fatigue behavior fatigue data analysis...
Abstract
Knowledge of fatigue behavior at the laminate level is essential for understanding the fatigue life of a laminated composite structure. This article describes fatigue failure of composite laminates in terms of layer cracking, delamination, and fiber break and interface debonding. It discusses the fatigue behavior of composite laminates in the form of a relation between applied maximum fatigue stress and fatigue life. The article explains Weibull distribution and parameters estimation for fatigue data analysis and life prediction of composite laminates. It analyzes the fatigue properties and damage tolerance of fiber-metal laminates such as ARALL and GLARE laminates. The article concludes with a discussion on the effects of fatigue on notched and unnotched specimens.
Book Chapter
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 December 1998
DOI: 10.31399/asm.hb.mhde2.a0003226
EISBN: 978-1-62708-199-3
..., and photography of fractured parts and surfaces, and describes some of the more common fractographic features revealed by light microscopy, including tensile-fracture surface marks in unnotched specimens, fatigue marks, and structural discontinuities within the metal. The article also explains how to interpret...
Abstract
Fractography is the systematic study of fractures and fracture surfaces. It is a useful tool in failure analysis and provides a means for correlating the influence of microstructure on the fracture mode of a given material. This article discusses the preservation, preparation, and photography of fractured parts and surfaces, and describes some of the more common fractographic features revealed by light microscopy, including tensile-fracture surface marks in unnotched specimens, fatigue marks, and structural discontinuities within the metal. The article also explains how to interpret fracture information contained in optical and scanning-electron microscope fractographs.
Image
in Properties of Wrought Aluminum and Aluminum Alloys
> Properties and Selection: Nonferrous Alloys and Special-Purpose Materials
Published: 01 January 1990
Image
in Properties of Wrought Aluminum and Aluminum Alloys
> Properties and Selection: Nonferrous Alloys and Special-Purpose Materials
Published: 01 January 1990
Fig. 8 Modified Goodman diagram for axial fatigue of unnotched specimens of alloy 2048-T851 plate
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Image
Published: 01 January 2005
Fig. 10 Delayed-failure characteristics of unnotched specimens of SAE 4340 steel during cathodic charging with hydrogen under standardized conditions. Electrolyte: 4% H 2 SO 4 in water. Poison: 5 drops/liter of cathodic poison composed of 2 g phosphorus dissolved in 40 mL CS 2 . Current
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Image
Published: 01 June 2024
Fig. 14 Schematics of crack initiation in unnotched and notched (drilled) specimens with rectangular cross sections. (a) Crack initiation at one corner and at the face of an unnotched specimen. (b) Crack initiation at one corner and at two corners in a drilled hole in a specimen. (c) Crack
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Image
Published: 01 January 1996
Fig. 11 Goodman diagram for the bending fatigue (R.R. Moore) of 8630 cast steel (normalized and tempered) for determining the fatigue limits in terms of cyclic stress range. The stress range (which is the difference between maximum and minimum stress) for unnotched specimens at zero mean
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Image
in Mechanisms and Appearances of Ductile and Brittle Fracture in Metals
> Failure Analysis and Prevention
Published: 01 January 2002
Fig. 28 Schematic of fracture surface regions in cylindrical tension-test specimens. (a) Surface from cone portion of fractured unnotched tensile specimen. (b) Surface of fractured notched specimen. Unlike the fracture surface for an unnotched specimen, the fracture surface for the notched
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Image
in Mechanisms and Appearances of Ductile and Brittle Fracture in Metals
> Failure Analysis and Prevention
Published: 15 January 2021
Fig. 28 Schematic of fracture-surface regions in cylindrical tension-test specimens. (a) Surface from cone portion of fractured unnotched tensile specimen. (b) Surface of fractured notched specimen. Unlike the fracture surface for an unnotched specimen, the fracture surface for the notched
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Image
Published: 01 December 2004
Fig. 18 Fracture surface regions in cylindrical tension-test specimens. (a) Surface from cone portion of fractured unnotched tensile specimen. (b) Surface of fractured notched specimen. Unlike the fracture surface for an unnotched specimen, the fracture surface for the notched specimen (b
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Image
Published: 01 January 1990
Fig. 3 Fatigue properties of two ferritic malleable irons (25 mm, or 1 in., diam bars) from bending fatigue tests on notched and unnotched specimens. The unnotched fatigue limit is about 200 MPa (29 ksi) for the iron with a 342 MPa (50 ksi) tensile strength and about 185 MPa (27 ksi
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Image
Published: 31 August 2017
Fig. 1 Fatigue properties of two ferritic malleable irons (25 mm, or 1 in., diam bars) from bending fatigue tests on notched and unnotched specimens. The unnotched fatigue limit is approximately 200 MPa (29 ksi) for the iron with a 342 MPa (50 ksi) tensile strength and approximately 185 MPa
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Image
Published: 01 January 1987
Fig. 63 Effect of a triaxial state of stress on the fracture mode in 13-8 pH stainless steel heat treated to an ultimate tensile strength of 1634 MPa (237 ksi). (a) and (b) Equiaxed dimples on the fracture surface of an unnotched specimen. (c) and (d) The quasi-cleavage fracture appearance
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Image
Published: 01 December 1998
Fig. 8 Reversed bending fatigue life at room temperature for gray iron containing 2.84% C, 1.52% Si, 1.05% Mn, 0.07% P, 0.12% S, 0.31% Cr, 0.20% Ni, and 0.37% Cu. Open circles represent notched specimens; closed circles represent unnotched specimens.
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Image
Published: 01 December 2008
Fig. 24 Effect of matrix structure on impact transition curves of ductile iron unnotched specimens. Source: Ref 38
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