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total length
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Image
Published: 01 March 2002
Fig. 9.13 Total crack length of microfissures in IN-718 plotted against grain size, showing that increased grain size leads to more cracking (microfissuring)
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Image
Published: 01 December 1995
Fig. 20-5a (a) Relationship between average total crack length at augmented strain and volume percent ferrite in the as-cast microstructure of 19Cr-9Ni-2.5Mo cast CF type steels. (b) Varestraint results for a substantially austenitic and a 7.6% ferrite bearing Ni-Cr-Mo cast CF-type steel
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Image
Published: 01 July 1997
Fig. 11 Plot of total crack length versus sulfur content as a function of two selected bulk carbon levels to show microfissuring susceptibility of cast alloy 718. Source: Ref 23
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Image
Published: 01 July 1997
Fig. 12 Plot of total crack length versus carbon content as a function of selected heat treatments for cast alloy 718 containing 0.009% S to show microfissuring susceptibility of the material
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Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2004
DOI: 10.31399/asm.tb.tt2.t51060195
EISBN: 978-1-62708-355-3
... standard, namely, product hardness; proof load by length measurement, yield strength, or uniform hardness; axial tension testing of full-sized products; wedge tension testing of full-sized products; tension testing of machined test specimens; and total extension at fracture testing. Finally, the chapter...
Abstract
This chapter focuses on tensile testing of three types of engineering components that undergo significant loading in tension, namely, threaded fasteners and bolted joints; adhesive joints; and welded joints. It describes the standardized tensile test for externally threaded fasteners and provides a brief background on relationships among torque, angle-of-turn, tension, and friction. The chapter also describes the test methods covered in the ASTM F 606M standard, namely, product hardness; proof load by length measurement, yield strength, or uniform hardness; axial tension testing of full-sized products; wedge tension testing of full-sized products; tension testing of machined test specimens; and total extension at fracture testing. Finally, the chapter covers tensile testing of adhesive and welded joints.
Image
Published: 01 December 2004
Fig. 1 Typical tensile specimen, showing a reduced gage section and enlarged shoulders. To avoid end effects from the shoulders, the length of the transition region should be at least as great as the diameter, and the total length of the reduced section should be at least four times
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Image
in Magnetic Field Imaging for Electrical Fault Isolation[1]
> Microelectronics Failure Analysis: Desk Reference
Published: 01 November 2019
Figure 36 3D XRM can provide additional details about the defect, such as shape, dimensions and thickness, The 3D reconstruction shows a planar view of the defect, total length of ≈ 180 µm by ≈ 45 µm (≈ 5 µm at the narrowest point). This view also reveals the relative position of the ROI
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Series: ASM Technical Books
Publisher: ASM International
Published: 01 August 2005
DOI: 10.31399/asm.tb.mmfi.t69540379
EISBN: 978-1-62708-309-6
... is then calculated using a i as the initial crack length. Final crack lengths can be estimated from fracture toughness or limit load calculations. The total fatigue life is obtained by summing the crack initiation and crack propagation lives. Note that a i is not based on actual fatigue mechanisms...
Abstract
This appendix presents an analytical model that estimates damage rates for both crack initiation and propagation mechanisms. The model provides a nonarbitrary definition of fatigue crack initiation length, which serves as an analytical link between initiation and propagation analyses and appears to have considerable merit in estimating the total fatigue life of notched and cracked structures.
Series: ASM Technical Books
Publisher: ASM International
Published: 01 October 2005
DOI: 10.31399/asm.tb.faesmch.t51270173
EISBN: 978-1-62708-301-0
... of an overhaul life of 550 hours. Visual Examination of General Physical Features The disc was found cracked close to the rim run-out radius, the crack penetrating through the thickness ( Fig. CH46.1 ). The total length of the cracked region was about 110 mm and, viewed on the diaphragm surface, the crack...
Abstract
A titanium alloy disc on the fourth stage of an aircraft engine compressor was found cracked in the course of a defect investigation. The disc had not yet reached the halfway point of its expected service life. The chapter explains how the crack was examined and provides relevant details about its location on the disc and various aspects of its appearance. It also explains how failure analysts concluded that the disc had been subjected to a fluctuating load of high magnitude and that the crack was the result of two fatigue cracks, originating from opposite sides of the diaphragm.
Image
Published: 01 December 1999
Fig. 5.36 Scatterbands for the tensile true fracture strain of a 0.4% C steel at three strength levels as a function of the total inclusion projected length in the fracture plane. Inclusions, total projected length. Source: Ref 58
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Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 October 2005
DOI: 10.31399/asm.tb.faesmch.t51270168
EISBN: 978-1-62708-301-0
... on one side only while the actual plate was countersunk on both sides. The total length of the locking screw should be 10.5 mm. The length of the hole drilled in the disc to accommodate the screws is 6.6 mm. With this design, with a locking plate of 3 mm thickness and a tab washer of 0.914 mm thickness...
Abstract
During cyclic spin tests, the turbine disc in an aircraft engine broke apart with a loud noise, followed by a fire. Based on a detailed examination and the results of SEM fractography and hardness measurements, failure analysts concluded that a locking plate became dislodged due to the shearing of the screws that hold it in place. They also provided recommendations to remediate the problem.
Image
Published: 01 December 1984
, 100 = 0.073 Lineal analysis L L α = Σ L α L T = Σ intercept lengths total line length = 152.3 2200 = 0.069 Point count P P α = Σ P α P T = Σ points in α total points = 5 + 2
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Image
in Evaluation of Stress-Corrosion Cracking[1]
> Stress-Corrosion Cracking: Materials Performance and Evaluation
Published: 01 January 2017
centerline within 1°. Bolt of material similar to specimen where practical; fine threaded, square, or Allen head. Thickness = B ; net width ( W ) = 2.55 B ; total width ( C ) = 3.20 B ; half height ( H ) = 1.24 B ; hole diameter ( D ) = 0.718 B + 0.003 B ; effective notch length ( M ) = 0.77 B ; notch
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Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2004
DOI: 10.31399/asm.tb.tt2.t51060001
EISBN: 978-1-62708-355-3
... Fig. 1 Typical tensile specimen, showing a reduced gage section and enlarged shoulders. To avoid end effects from the shoulders, the length of the transition region should be at least as great as the diameter, and the total length of the reduced section should be at least four times...
Abstract
Tensile tests are performed for several reasons related to materials development, comparison, selection, and quality control. The properties derived from tensile tests are used in selecting materials for engineering applications. Tensile properties often are used to predict or estimate the behavior of a material under forms of loading other than uniaxial tension. This chapter provides a brief overview of tensile specimens and test machines, stress-strain curves, true stress and strain, and test methodology and data analysis.
Series: ASM Technical Books
Publisher: ASM International
Published: 01 August 2012
DOI: 10.31399/asm.tb.smff.t53400027
EISBN: 978-1-62708-316-4
... of 10 –1 to 10 0 ( Ref 3.2 ). As a result, the total strain can be described by: (Eq 3.3) e ≈ e pl since e el ≪ e pl Thus, for the final length, ℓ 1 , after removal of the force, (Eq 3.4) e pl = ℓ 1 − ℓ 0...
Abstract
This chapter discusses the fundamentals of plastic deformation and the role of strain and strain rate in sheet metal forming processes. It describes the conditions associated with uniform deformation, the significance of engineering and true strain, the effect of volume constancy on the tensile response of isotropic and anisotropic materials, and how infinitesimal strains or strain rates are used to express and analyze instantaneous deformation and local stain. It also discusses the concept of principal strain and strain paths and explains how to determine, and when to use, equivalent strain and strain rate.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2004
DOI: 10.31399/asm.tb.tt2.t51060155
EISBN: 978-1-62708-355-3
... complete. It is possible to measure the total length of the original reference dimension and calculate how much longer the total length of the two separate sections is. This is expressed as a percentage. Some elastomers will exhibit almost total recovery, whereas others may display tension set as high...
Abstract
Elastomers comprise a subclass of polymers that display the ability to stretch and recover that is typical of a rubber band. This chapter describes the properties determined by tensile testing of elastomers and the factors influencing them, namely, structuring of the molecular matrix, compounding, specimen preparation, specimen type, vulcanization parameters, and temperature. The chapter also provides information on ASTM D 412, the most widely referenced standard for determining the tensile properties of elastomers.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 1984
DOI: 10.31399/asm.tb.mpp.t67850410
EISBN: 978-1-62708-260-0
... by the International Society for Stereology Symbol Units Description Common name P Number of point elements or test points P p Point fraction, i.e., number of point elements per total number of test points Point count L mm Length of linear elements or test line length P L mm...
Abstract
This chapter covers the emerging practice of quantitative microscopy and its application in the study of the microstructure of metals. It describes the methods used to quantify structural gradients, volume fraction, grain size and distribution, and other features of interest. It provides examples showing how the various features appear, how they are measured, and how the resulting data are converted into usable form. The chapter also discusses the quantification of fracture morphology and its correlation with material properties and behaviors.
Image
Published: 01 December 1999
Fig. 5.41 Relationship between the limiting fatigue stress in smooth, rotating bending tests and total inclusion projected length. Results for two test orientations and three strength levels are shown. Source: Ref 58
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Image
in Mechanisms of Stress-Corrosion Cracking[1]
> Stress-Corrosion Cracking: Materials Performance and Evaluation
Published: 01 January 2017
Fig. 1.29 Typical subcritical crack propagation rate vs. stress-intensity relationship. Stress intensity, K , is defined as K = A σ π C / B , where σ is the total tensile stress, C is the crack length, and A and B are geometrical constants.
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Image
Published: 01 December 2015
Fig. 26 Typical, subcritical crack propagation rate versus stress intensity relationship. Stress intensity, K , is defined as K = A σ π C / B , where s is the total tensile stress, C is the crack length, and A and B are geometrical constants.
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